Relevant bibliographies by topics / Missile Antennas

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Missile Antennas'

Author: Grafiati
Published: 4 June 2021
Last updated: 15 February 2022

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Journal articles on the topic "Missile Antennas"

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Wang, Wei, Xue Tian Wang, Ying Li, and Song Song. "Design of an Ultra-Wideband Four Arms Sinuous Antenna." Advanced Materials Research 981 (July 2014): 469–73. http://dx.doi.org/10.4028/www.scientific.net/amr.981.469.

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Due to the advantages of ultra-wideband, single caliber, symmetric pattern, full polarization, the sinuous antennas have gradually displaced the traditional spiral antennas in the Missile guider, reflector feed, wideband direction finding system. Based on the traditional planar sinuous antennas, this paper designed a novel 2-22 GHz 3D sinuous antenna in the conical form. Results show that the designed antenna showed high performance within 2-22 GHZ frequency band.
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Gonçalves, André Paim, Renan Miranda Richter, Felipe Streitenberger Ivo, Alessandro Roberto Santos, Robson Ribeiro Carreira, and Olympio Lucchini Coutinho. "Proposal of anti-radiation missile decoy assisted by microwave photonics." Revista Brasileira de Aplicações de Vácuo 39, no. 3 (December 28, 2020): 218–23. http://dx.doi.org/10.17563/rbav.v39i3.1178.

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This article has proposed the concept of a decoy that could be used against anti-radiation missiles (ARMs). The bait signals are generated remotely and transmitted to the sacrificial antenna site over a fiber-optic network. This network has the possibility to support broadband radar signals in the range of a few GHz. This study postulated a distance of 1 km in relation to its park of antennas, distance that may be greater. This analog fiber link was designed for radar signal transmission in the frequency range of 0.3 to 3 GHz. The theoretical results were compared with the experimental ones, and it was observed that the behavior of the radar signal power gained in the studied range is straight. Thus, the signal does not present distortions. The system proposed in this study is promising as a distraction for ARMs.
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Vyas, Kirti, Garima Sanyal, Arun Kumar Sharma, and Pramod Kumar Singhal. "Gain enhancement over a wideband in CPW-fed compact circular patch antenna." International Journal of Microwave and Wireless Technologies 6, no. 5 (December 13, 2013): 497–503. http://dx.doi.org/10.1017/s1759078713001037.

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The present paper reports the gain enhancement over a wideband (12–15 GHz) in a coplanar waveguide (CPW)-fed circular patch antenna with circular defected ground structure (DGS). Two compact coplanar circular antennas have been designed and fabricated with and without DGS of same volume 18 × 20 × 1.6 mm3, built over FR4-epoxy substrate (εr = 4.4). Gain enhancement has been achieved by optimizing the current distribution with suitable DGS. For this purpose, structural designs have been optimized by parametric simulations in HFSS and CST MWS. Both the antennas can perform well in variety of wireless communication including WLAN IEEE 802.11 g/a (5.15–5.35 GHz and 5.725–5.825 GHz) and X-band applications including short range, tracking, missile guidance, and radar communication that ranges roughly from 8.29 to 11.4 GHz. The measured experimental results show that impedance bandwidth (S11 < −10 dB) of antenna with DGS is 100%. The antenna with DGS offers gain improvement by 2.7 dB for 13 GHz and 7 dB for 14 GHz. The performance of antenna with DGS is compared to conventional CPW-fed circular patch antenna (without DGS) in terms of reflection coefficient, radiation characteristics, and gain.
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Biswas, Diptiman, and Asif Rizwan. "Frustum Shaped Conformal Antenna for Spinning Aerial Platform." Defence Science Journal 68, no. 4 (June 26, 2018): 388. http://dx.doi.org/10.14429/dsj.68.12217.

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<p>A novel approach to design and develop frustum shaped conformal antenna for transmission of telemetry data from a missile like spinning aerial platform is described. The requirement necessitates for an omni directional radiation pattern in the roll plane. However, the criteria is not feasible to achieve by using a monopole or a dipole as the omni coverage due to these antennas are restricted only in yaw or azimuth plane of the aerial platform. A conformal antenna appropriately wrapped on to the surface provides potential solution and accordingly has been configured for meeting the requirements of a practical application. The antenna artwork has been designed to conform to the exterior geometry of the intended portion of conical surface and printed on a microwave substrate which is essentially thin and flexible. A corporate feed distribution scheme has been designed and tailored to match with the impedance of the microstrip radiator at multiple locations and also printed along with it making the frustum antenna very compact and of aerodynamic supportive form. The antenna produces required omni coverage in the plane normal to the roll axis. A step-wise method for the design and development of the frustum conformal antenna through simulation and experiment approach has been discussed.</p>
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Andreev, А. "Outlook for application of radars with phased-array antennas in foreign navies on missile tracking ships." Transactions of the Krylov State Research Centre 3, no. 385 (August 27, 2018): 145–52. http://dx.doi.org/10.24937/2542-2324-2018-3-385-145-152.

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Lohn, Jason D., Gregory S. Hornby, and Derek S. Linden. "Human-competitive evolved antennas." Artificial Intelligence for Engineering Design, Analysis and Manufacturing 22, no. 3 (June 12, 2008): 235–47. http://dx.doi.org/10.1017/s0890060408000164.

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AbstractWe present a case study showing a human-competitive design of an evolved antenna that was deployed on a NASA spacecraft in 2006. We were fortunate to develop our antennas in parallel with another group using traditional design methodologies. This allowed us to demonstrate that our techniques were human-competitive because our automatically designed antenna could be directly compared to a human-designed antenna. The antennas described below were evolved to meet a challenging set of mission requirements, most notably the combination of wide beamwidth for a circularly polarized wave and wide bandwidth. Two evolutionary algorithms were used in the development process: one used a genetic algorithm style representation that did not allow branching in the antenna arms; the second used a genetic programming style tree-structured representation that allowed branching in the antenna arms. The highest performance antennas from both algorithms were fabricated and tested, and both yielded very similar performance. Both antennas were comparable in performance to a hand-designed antenna produced by the antenna contractor for the mission, and so we consider them examples of human-competitive performance by evolutionary algorithms. Our design was approved for flight, and three copies of it were successfully flown on NASA's Space Technology 5 mission between March 22 and June 30, 2006. These evolved antennas represent the first evolved hardware in space and the first evolved antennas to be deployed.
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Tan, Chee Leong, and Hooman Mohseni. "Emerging technologies for high performance infrared detectors." Nanophotonics 7, no. 1 (January 1, 2018): 169–97. http://dx.doi.org/10.1515/nanoph-2017-0061.

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AbstractInfrared photodetectors (IRPDs) have become important devices in various applications such as night vision, military missile tracking, medical imaging, industry defect imaging, environmental sensing, and exoplanet exploration. Mature semiconductor technologies such as mercury cadmium telluride and III–V material-based photodetectors have been dominating the industry. However, in the last few decades, significant funding and research has been focused to improve the performance of IRPDs such as lowering the fabrication cost, simplifying the fabrication processes, increasing the production yield, and increasing the operating temperature by making use of advances in nanofabrication and nanotechnology. We will first review the nanomaterial with suitable electronic and mechanical properties, such as two-dimensional material, graphene, transition metal dichalcogenides, and metal oxides. We compare these with more traditional low-dimensional material such as quantum well, quantum dot, quantum dot in well, semiconductor superlattice, nanowires, nanotube, and colloid quantum dot. We will also review the nanostructures used for enhanced light-matter interaction to boost the IRPD sensitivity. These include nanostructured antireflection coatings, optical antennas, plasmonic, and metamaterials.
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Hornby, Gregory S., Jason D. Lohn, and Derek S. Linden. "Computer-Automated Evolution of an X-Band Antenna for NASA's Space Technology 5 Mission." Evolutionary Computation 19, no. 1 (March 2011): 1–23. http://dx.doi.org/10.1162/evco_a_00005.

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Whereas the current practice of designing antennas by hand is severely limited because it is both time and labor intensive and requires a significant amount of domain knowledge, evolutionary algorithms can be used to search the design space and automatically find novel antenna designs that are more effective than would otherwise be developed. Here we present our work in using evolutionary algorithms to automatically design an X-band antenna for NASA's Space Technology 5 (ST5) spacecraft. Two evolutionary algorithms were used: the first uses a vector of real-valued parameters and the second uses a tree-structured generative representation for constructing the antenna. The highest-performance antennas from both algorithms were fabricated and tested and both outperformed a hand-designed antenna produced by the antenna contractor for the mission. Subsequent changes to the spacecraft orbit resulted in a change in requirements for the spacecraft antenna. By adjusting our fitness function we were able to rapidly evolve a new set of antennas for this mission in less than a month. One of these new antenna designs was built, tested, and approved for deployment on the three ST5 spacecraft, which were successfully launched into space on March 22, 2006. This evolved antenna design is the first computer-evolved antenna to be deployed for any application and is the first computer-evolved hardware in space.
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Ge, Lei, Xujun Yang, Zheng Dong, Dengguo Zhang, and Xierong Zeng. "Reconfigurable Magneto-Electric Dipole Antennas for Base Stations in Modern Wireless Communication Systems." Wireless Communications and Mobile Computing 2018 (2018): 1–8. http://dx.doi.org/10.1155/2018/2408923.

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Magneto-electric (ME) dipole antennas, with the function of changing the antenna characteristics, such as frequency, polarization, or radiation patterns, are reviewed in this paper. The reconfigurability is achieved by electrically altering the states of diodes or varactors to change the surface currents distributions or reflector size of the antenna. The purpose of the designs is to obtain agile antenna characteristics together with good directive radiation performances, such as low cross-polarization level, high front-to-back ratio, and stable gain. By reconfiguring the antenna capability to support more than one wireless frequency standard, switchable polarizations, or cover tunable areas, the reconfigurable ME dipole antennas are able to switch functionality as the mission changes. Therefore, it can help increase the communication efficiency and reduce the construction cost. This shows very attractive features in base station antennas of modern wireless communication applications.
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Kogan, L. R. "Position Angle of the HALCA Antenna Feed." International Astronomical Union Colloquium 164 (1998): 419–20. http://dx.doi.org/10.1017/s0252921100046224.

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AbstractKnowledge of the position angle of an antenna feed is very important for polarization observations. The issue had been developed for ground based antennas but has not been considered for a orbiting antennas. We provide a calculation of the position angle of the Japanese satellite VSOP/HALCA which was successfully launched in a space VLBI mission.
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Dissertations / Theses on the topic "Missile Antennas"

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Vines, Roger. "MISSILE ANTENNA PATTERNS FOR WIDELY-SPACED MULTI-ELEMENT ARRAYS." International Foundation for Telemetering, 2005. http://hdl.handle.net/10150/605040.

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ITC/USA 2005 Conference Proceedings / The Forty-First Annual International Telemetering Conference and Technical Exhibition / October 24-27, 2005 / Riviera Hotel & Convention Center, Las Vegas, Nevada
Multiple discrete antennas distributed around the circumference of a large missile and driven by one transmitter are sometimes used to radiate telemetry omnidirectionally. But driving discrete antennas separated by several wavelengths around the missile body with a single transmitter can result in an antenna pattern with deep nulls in the roll plane. Varying the relative signal phase or amplitude among the signals driving the antennas as well as the polarization of the antennas can be used to change the nulls in an attempt to decrease the null depth. In this paper the effects of phase, amplitude, and polarization on the roll-plane pattern are examined and measurement data presented.
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Esswein, Lance C. "Genetic algorithm design and testing of a random element 3-D 2.4 GHZ phased array transmit antenna constructed of commercial RF microchips." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03Jun%5FEsswein.pdf.

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Thesis (M.S. in Physics)--Naval Postgraduate School, June 2003.
Thesis advisor(s): Michael Melich, David Jenn, Rodney Johnson. Includes bibliographical references (p. 113-115). Also available online.
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Fischer, Andrew Cassidy. "Conformal Microstrip GPS Antenna for Missile Application." DigitalCommons@CalPoly, 2011. https://digitalcommons.calpoly.edu/theses/510.

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Optimal missile guidance and flight performance require accurate and continuously updated in-flight coordinate data. The Global Positioning System (GPS) is used for this positional awareness. However, due to missile rotation and orientation variations during flight, GPS signal reception using traditional antennas may be intermittent. To remain cost competitive, Stellar Exploration Inc. is developing a low-cost omnidirectional GPS antenna for guided missile prototypes. In this thesis, existing products and design techniques are examined, design constraints for supersonic missile applications are investigated, and corresponding performance goals are established. A conformal microstrip patch antenna is developed and simulated in Agilent’s Advanced Design System (ADS). The resulting antenna is constructed and characterized. Prototype testing verifies that the antenna maintains GPS signal lock regardless of orientation. The final cost is significantly lower than existing conformal products. A second revision investigates enhanced modeling, dimensional reductions (via increased dielectric constant), and radome construction. Performance is compared to first revision antenna results and differences are examined. Suggestions for further revisions are discussed.
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Kjellberg, Malin. "Stabilizing a missile radar antenna Using Axiomatic Design." Thesis, KTH, Maskinkonstruktion (Inst.), 2007. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-100712.

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This thesis work describes a brand new concept of how to, from a mechanical perspective, stabilize/mount a radar antenna. The antenna must be able to rotate ±60 degrees around pitch and yaw without disturbing the radar characteristics. At the same time the antenna diameter must be as large as possible to enhance radar quality. Axiomatic Design was applied as the work method which helped developing a brand new concept of how to mount the antenna. This concept study was made for Saab Bofors Dynamics at Massachusetts Institute of Technology in the lab ”Park Centre for Complex Systems” under supervision of Prof. Nam P. Suh (MIT) and Jan-Gunnar Persson (KTH). The invention process using Axiomatic Design resulted in a brand new concept. A fixed sphere, in which the antenna can slide, eliminates the translational degrees of freedom. Two linkages actuate the antenna by means of linear motors. A careful selection of joints eliminates the last unwanted degree of freedom. Left are two rotational DOF, one around pitch and one around yaw. Only the thickness of the sphere and the missile inner diameter limit the size of the antenna diameter. The radar disturbance is remaining low, since the additional disturbance is very low and the same in every angle in the ±60 degree of freedom that the antenna has. That is achieved by letting the antenna slide inside a sphere where the walls are equally thick all around the required work space. The material of the sphere could preferably be the same as in the radome. Oversteering is minimized since direct drive is possible. No transmission is needed. The antenna has physical restrictions at 90 degrees. Since that is outside the work space it does not affect the rotation mechanism.
Denna rapport beskriver en konseptstudie på hur man på olika sätt kan rotera en två frihetsgraders radarantenn. Antennen har rörelsekrav på ±60 grader kring tilt samt elevation. Den ska placeras inuti en missil, vilket ger den utrymmesrestriktioner. För att optimera antennens kvalitet får antennens microvågor störas minimalt samtidigt som antennens diameter måste vara så stor som möjligt. Axiomatic Design har tillämpats som utvecklingsmetod för att komma fram till ett konstuktionskoncept. Denna konseptstudie har utförts för Saab Bofors Dynamics vid Massachusetts Institute of Technology, MIT under ledning av Håkan Skytt (Saab Bofors Dynamics) och Nam P. Suh (MIT) och Jan-Gunnar Persson (KTH). Efter att ha värderat olika lösningsförslag med hjälp av Axiomatic Design valdes ett koncept refererat som Fixed Sphere. Antennen slider m h a lågfriktionsytor inuti en sfär. Två länkar med linjära motorer i respektive länk vrider antennen. Noggrant utvalda leder begränsar antalet frihetsgrader hos antennen till de önskade frihetsgraderna. Sfären maximerar storleken hos antennen. Bara sfärens väggtjocklek, samt missilens yttervägg begränsar antennens diameter. Mikrovågorna, vars kvalitet är av yttersta vikt, försämras marginellt då samma typ av material väljs som används till radomen på missilen. Sfärens geometri gör att den tillkomna störningen är konstant, oavsett hur antennen vrider sig inom arbetsområdet ±60 grader. Detta är åstadkommet genom att väggtjockleken är konstant genom hela arbetsområdet. Det gör att mängden material m a o väggtjockleken som radarn ser igenom är konstant oavsett vinkel. Överstyrdheten hos radarn antas elimineras då motorerna kan direktköras. Det finns inga kugghjul som kan skapa och sprida glapp. Rörlighetsförmågan hos antennen har restriktioner kring ±90 grader, men då detta ligger utanför arbetsområdet kan det bortses ifrån.
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Ribardière, Patrick. "Contribution à l'étude de la diminution de la surface équivalente radar d'aéronefs par une méthode active." Limoges, 1993. http://www.theses.fr/1993LIMO0210.

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Ce memoire presente une etude theorique d'un systeme actif de reduction de la surface equivalente radar (s. E. R. ) monostatique de missiles, supposes parfaitement conducteurs, dans leur zone de resonance. L'analyse du comportement electromagnetique d'un mobile face a une onde radar incidente est tout d'abord effectuee. La methode de resolution d'un tel probleme est basee sur l'etude de la diffraction d'ondes electromagnetiques par des structures conductrices en regime transitoire. Le champ electromagnetique diffracte par une cible est calcule en zone proche par une methode aux differences finies, l'application du principe d'huygens permet ensuite de determiner le champ a grande distance, et d'en deduire la s. E. R. . L'outil numerique a ete valide en confrontant les resultats a des resultats experimentaux ou theoriques utilisant des methodes differentes. Le principe de reduction de la s. E. R. Propose repose sur le pilotage de quatre antennes plaquees reparties sur le missile. L'application en temps reel de puissances et phases adequates a chacune de ces antennes permet de generer dans la direction du radar un champ electromagnetique en opposition de phase avec celui diffracte par le missile dans la meme direction. La modelisation numerique du mobile muni de ses antennes a permis de calculer les caracteristiques des alimentations permettant une annulation de la surface equivalente radar monastatique de la structure sans demander aux generateurs des puissances disponibles prohibitives. L'etude de la sensibilite des resultats a diverses sources sources d'erreurs a montre l'attention qui devra etre apportee aux mesures et calculs des differents parametres du systeme de compensation de la s. E. R.
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Cirineo, Tony, Rick Davis, Marvin Byrd, and Scott Kujiraoka. "Design and Development of a Thin Conformal C-Band Telemetry Antenna for a Small Diameter Missile." International Foundation for Telemetering, 2011. http://hdl.handle.net/10150/595618.

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ITC/USA 2011 Conference Proceedings / The Forty-Seventh Annual International Telemetering Conference and Technical Exhibition / October 24-27, 2011 / Bally's Las Vegas, Las Vegas, Nevada
This paper will present the preliminary design of a C-Band telemetry antenna mounted conformal to a small diameter missile. Various design studies and options will be explored leading to a preliminary design that best meets system requirements. Simulation results are presented for various options and the rationale for down selection to final configuration is discussed.
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Abouzahra, Mohamed D., Bill Patton, Guy Tarnstrom, and Dana Wells. "TELEMETRY MODERNIZATION AT THE KWAJALEIN MISSILE RANGE." International Foundation for Telemetering, 2001. http://hdl.handle.net/10150/606454.

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International Telemetering Conference Proceedings / October 22-25, 2001 / Riviera Hotel and Convention Center, Las Vegas, Nevada
Telemetry support has been a component of the instrumentation test support structure at Kwajalein Missile Range (KMR) for nearly 40 years. From a limited initial suite of manually pointed telemetry antennas, the Range has grown to include nine tracking antennas and four fixed receiving antennas. This paper describes the current modernization program at KMR that will include nine new telemetry trackers and five fixed antennas that will be networked and controlled via fiber optic links from a newly established telemetry control center on the island of Kwajalein. These upgrades will reduce operational cost and institute efficiencies, while continuing to meet Range Users’ growing requirements.
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Tong, Chin Hong Matthew. "System study and design of broad-band U-Slot microstrip patch antennas for aperstructures and opportunistic arrays." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2005. http://library.nps.navy.mil/uhtbin/hyperion/05Dec%5FTong.pdf.

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Thesis (M.S. in Combat Systems Technology)--Naval Postgraduate School, December 2005.
Thesis Advisor(s): David C. Jenn, Donald L. Walters. Includes bibliographical references (p.83-85). Also available online.
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Kujiraoka, Scott R. "USING COMMERCIAL-OFF-THE-SHELF (COTS) PRODUCTS IN THE DESIGN OF MISSILE FLIGHT-QUALIFIED HARDWARE." International Foundation for Telemetering, 2001. http://hdl.handle.net/10150/607685.

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International Telemetering Conference Proceedings / October 22-25, 2001 / Riviera Hotel and Convention Center, Las Vegas, Nevada
During these times of acquisition reform in the federal government, various missile systems are being forced into using Commercial-off-the-Shelf (COTS) products in the design of their subsystems. However one problem that this presents is the lack of configuration management. There is a concern that the manufacturer will modify the product without informing the end user. This may have a severe effect on the performance of an already flight qualified subsystem. An example of how one program is dealing with this issue will be discussed.
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Kujiraoka, Scott, Russell Fielder, Johnathan Jones, and Aliva Sandberg. "Latest Status on Adding FTS Capability to a Missile Telemetry Section." International Foundation for Telemetering, 2010. http://hdl.handle.net/10150/605940.

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ITC/USA 2010 Conference Proceedings / The Forty-Sixth Annual International Telemetering Conference and Technical Exhibition / October 25-28, 2010 / Town and Country Resort & Convention Center, San Diego, California
Development is currently underway to produce a dual redundant Flight Termination System (FTS) capable Missile Telemetry Section. This FTS will mainly consist of a conformal wraparound antenna, two flight termination safe & arm (FTS&A) devices, two flight termination receivers (FTR), two explosive foil initiators (EFI) and destruct charge. This paper will discuss the current status of the development of these FTS components along with the process of obtaining the Flight Certification from Range and System Safety to fly this newly outfitted missile on a governmental test range.
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Books on the topic "Missile Antennas"

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Rogers, Craig A. Large deployable antenna program: Phase I: Technology assessment and mission architecture. Hampton, Va: Langley Research Center, 1991.

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Schneider, W. C. 29th Aerospace Mechanics Symposium: Proceedings of a symposium held at the South Shore Harbour Resort and Conference Center, League City, Texas and co-sponsored by NASA Johnson Space Center and Lockheed Missiles and Space Company, Inc, May 17-19, 1995. Houston, Texas: Lyndon B. Johnson Space Center, 1995.

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Radiation Pattern Calculation for Missile Radomes in the Near Field of an Antenna. Storming Media, 1996.

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Book chapters on the topic "Missile Antennas"

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Jobanputra, Ami, Dhruv Panchal, Het Trivedi, Dhyey Buch, and Bhavin Kakani. "Development of Antennas Subsystem for Indian Airborne Cruise Missile." In Proceedings of the International Conference on Paradigms of Computing, Communication and Data Sciences, 619–29. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-7533-4_49.

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James, D. A. "Seeker Antenna Systems." In Radar Homing Guidance for Tactical Missiles, 38–55. London: Macmillan Education UK, 1986. http://dx.doi.org/10.1007/978-1-349-08602-3_4.

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Shi, Chuang, Ludwig Grunwaldt, Jean-Claude Raimondo, Franz-Heinrich Massmann, and Sheng Yuan Zhu. "Determination of the Offset of CHAMP GPS Antenna with Respect to Satellite’s Mass Center." In First CHAMP Mission Results for Gravity, Magnetic and Atmospheric Studies, 38–41. Berlin, Heidelberg: Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-540-38366-6_6.

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Lohn, Jason D., Gregory S. Hornby, and Derek S. Linden. "Evolution, Re-evolution, and Prototype of an X-Band Antenna for NASA’s Space Technology 5 Mission." In Evolvable Systems: From Biology to Hardware, 205–14. Berlin, Heidelberg: Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/11549703_20.

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Khare, Bharat Bhushan, Akash Kumar Bhoi, Sanjeev Sharma, and Akanksha Lohia. "Missile Structured Wearable Antenna for Power Harvesting Application." In Design and Optimization of Sensors and Antennas for Wearable Devices, 127–38. IGI Global, 2020. http://dx.doi.org/10.4018/978-1-5225-9683-7.ch011.

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In this chapter, a single element of wearable antenna is designed, and further, to enhance the gain, a wearable rectenna array is designed that can be utilized for the purpose of energy harvesting at 3.14 GHz. The theoretical analysis of received power has been studied. The anticipated antenna array shows the directivity of 8.048 dBi that was used to calculate received power by antenna array at the distance of 10 meters from transmitter. This rectenna array can be used to operate the micro-electronic gadgets and to operate small sensors.
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"ESA Deep Space Antenna 2 Pointing Calibration System." In Space Operations: Mission Management, Technologies, and Current Applications, 201–16. Reston ,VA: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/5.9781600866890.0201.0216.

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El-Said, Mostafa. "A Bio-Inspired Approach for the Next Generation of Cellular Systems." In Mobile Computing, 3204–10. IGI Global, 2009. http://dx.doi.org/10.4018/978-1-60566-054-7.ch236.

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In the current 3G systems and the upcoming 4G wireless systems, missing neighbor pilot refers to the condition of receiving a high-level pilot signal from a Base Station (BS) that is not listed in the mobile receiver’s neighbor list (LCC International, 2004; Agilent Technologies, 2005). This pilot signal interferes with the existing ongoing call, causing the call to be possibly dropped and increasing the handoff call dropping probability. Figure 1 describes the missing pilot scenario where BS1 provides the highest pilot signal compared to BS1 and BS2’s signals. Unfortunately, this pilot is not listed in the mobile user’s active list. The horizontal and vertical handoff algorithms are based on continuous measurements made by the user equipment (UE) on the Primary Scrambling Code of the Common Pilot Channel (CPICH). In 3G systems, UE attempts to measure the quality of all received CPICH pilots using the Ec/Io and picks a dominant one from a cellular system (Chiung & Wu, 2001; El-Said, Kumar, & Elmaghraby, 2003). The UE interacts with any of the available radio access networks based on its memorization to the neighboring BSs. As the UE moves throughout the network, the serving BS must constantly update it with neighbor lists, which tell the UE which CPICH pilots it should be measuring for handoff purposes. In 4G systems, CPICH pilots would be generated from any wireless system including the 3G systems (Bhashyam, Sayeed, & Aazhang, 2000). Due to the complex heterogeneity of the 4G radio access network environment, the UE is expected to suffer from various carrier interoperability problems. Among these problems, the missing neighbor pilot is considered to be the most dangerous one that faces the 4G industry. The wireless industry responded to this problem by using an inefficient traditional solution relying on using antenna downtilt such as given in Figure 2. This solution requires shifting the antenna’s radiation pattern using a mechanical adjustment, which is very expensive for the cellular carrier. In addition, this solution is permanent and is not adaptive to the cellular network status (Agilent Technologies, 2005; Metawave, 2005).
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El-Said, M. "Bio-Inspired Approach for the Next Generation of Cellular Systems." In Encyclopedia of Mobile Computing and Commerce, 63–67. IGI Global, 2007. http://dx.doi.org/10.4018/978-1-59904-002-8.ch011.

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Abstract:
In the current 3G systems and the upcoming 4G wireless systems, missing neighbor pilot refers to the condition of receiving a high-level pilot signal from a Base Station (BS) that is not listed in the mobile receiver’s neighbor list (LCC International, 2004; Agilent Technologies, 2005). This pilot signal interferes with the existing ongoing call, causing the call to be possibly dropped and increasing the handoff call dropping probability. Figure 1 describes the missing pilot scenario where BS1 provides the highest pilot signal compared to BS1 and BS2’s signals. Unfortunately, this pilot is not listed in the mobile user’s active list. The horizontal and vertical handoff algorithms are based on continuous measurements made by the user equipment (UE) on the Primary Scrambling Code of the Common Pilot Channel (CPICH). In 3G systems, UE attempts to measure the quality of all received CPICH pilots using the Ec/Io and picks a dominant one from a cellular system (Chiung & Wu, 2001; El-Said, Kumar, & Elmaghraby, 2003). The UE interacts with any of the available radio access networks based on its memorization to the neighboring BSs. As the UE moves throughout the network, the serving BS must constantly update it with neighbor lists, which tell the UE which CPICH pilots it should be measuring for handoff purposes. In 4G systems, CPICH pilots would be generated from any wireless system including the 3G systems (Bhashyam, Sayeed, & Aazhang, 2000). Due to the complex heterogeneity of the 4G radio access network environment, the UE is expected to suffer from various carrier interoperability problems. Among these problems, the missing neighbor pilot is considered to be the most dangerous one that faces the 4G industry. The wireless industry responded to this problem by using an inefficient traditional solution relying on using antenna downtilt such as given in Figure 2. This solution requires shifting the antenna’s radiation pattern using a mechanical adjustment, which is very expensive for the cellular carrier. In addition, this solution is permanent and is not adaptive to the cellular network status (Agilent Technologies, 2005; Metawave, 2005).Therefore, a self-managing solution approach is necessary to solve this critical problem. Whisnant, Kalbarczyk, and Iyer (2003) introduced a system model for dynamically reconfiguring application software. Their model relies on considering the application’s static structure and run-time behaviors to construct a workable version of reconfiguration software application. Self-managing applications are hard to test and validate because they increase systems complexity (Clancy, 2002). The ability to reconfigure a software application requires the ability to deploy a dynamically hardware infrastructure in systems in general and in cellular systems in particular (Jann, Browning, & Burugula, 2003).
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Conference papers on the topic "Missile Antennas"

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Xuegang Zeng and Weigan Lin. "Radar equation and signal design for the electromagnetic missile." In IEEE Antennas and Propagation Society International Symposium 1992 Digest. IEEE, 1992. http://dx.doi.org/10.1109/aps.1992.221995.

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Qiao Xiaolin, Jin Ming, and Song Lizhong. "Design of a new dual-polarization antenna on missile." In 6th International SYmposium on Antennas, Propagation and EM Theory, 2003. Proceedings. 2003. IEEE, 2003. http://dx.doi.org/10.1109/isape.2003.1276653.

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Jun, Zhang, Wang Wen-Peng, and Fan Qing-Hui. "The study of effective accumulation algorithm of the missile-borne chirp radar." In 2014 3rd Asia-Pacific Conference on Antennas and Propagation. IEEE, 2014. http://dx.doi.org/10.1109/apcap.2014.6992774.

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Chen, Cong, Jiebo Li, Lin Zhang, and Haitao Chen. "Research of the missile and aircraft base mounted antennas for data transmission." In 2010 International Conference on Microwave and Millimeter Wave Technology (ICMMT). IEEE, 2010. http://dx.doi.org/10.1109/icmmt.2010.5524978.

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Jun-chao, Yuan, and Zhang Xiao-kuan. "Research on RCS time series of ballistic missile warhead in reentry phase." In 2016 11th International Symposium on Antennas, Propagation and EM Theory (ISAPE). IEEE, 2016. http://dx.doi.org/10.1109/isape.2016.7834063.

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Jacobs, J. P., and W. P. du Plessis. "High-accuracy Gaussian process modelling of missile RCS with cost-based preferential training data selection." In 12th European Conference on Antennas and Propagation (EuCAP 2018). Institution of Engineering and Technology, 2018. http://dx.doi.org/10.1049/cp.2018.1253.

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Qiu Qi-Ming, Zhang Lin-Rang, and Yi Yu-Sheng. "Study on Ship-Formation Detection by Missile-Borne Radar using DBS Imaging Algorithm." In 2008 8th International Symposium on Antennas, Propagation & EM Theory (ISAPE - 2008). IEEE, 2008. http://dx.doi.org/10.1109/isape.2008.4735298.

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Liang, Yu, Xiang-hua Zeng, Li-xin Guo, and Zhen-sen Wu. "A study of composite electromagnetic scattering from rough sea surface and missile-like target basing on the efficient numerical algorithm." In 2014 3rd Asia-Pacific Conference on Antennas and Propagation. IEEE, 2014. http://dx.doi.org/10.1109/apcap.2014.6992690.

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Lee, Hung-Mou. "On Wu's electromagnetic missile." In 1986 Symposium on Antenna Technology and Applied Electromagnetics. IEEE, 1986. http://dx.doi.org/10.1109/antem.1986.7856367.

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Yigit, Olcay, Yavuz Asci, and Korkut Yegin. "Dual band GNSS antenna for missile applications." In 2018 22nd International Microwave and Radar Conference (MIKON). IEEE, 2018. http://dx.doi.org/10.23919/mikon.2018.8405160.

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Reports on the topic "Missile Antennas"

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Polcawich, Ronald G., Daniel Judy, Jeff Pulskamp, Steve Weiss, Janice Rock, and Tracy Hudson. U.S. Army Research Laboratory Microelectromechanical System Electronically Scanned Antenna Testing at the Aviation and Missile Research, Development and Engineering Center. Fort Belvoir, VA: Defense Technical Information Center, January 2008. http://dx.doi.org/10.21236/ada476489.

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