Relevant bibliographies by topics / Perigee and Apogee radius

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  2. Dissertations / Theses
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Academic literature on the topic 'Perigee and Apogee radius'

Author: Grafiati
Published: 4 June 2025
Last updated: 15 July 2025

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Journal articles on the topic "Perigee and Apogee radius"

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N., Gayathri, and Mahalakshmi S. "A Study on Orbital Mechanics." International Journal of Trend in Scientific Research and Development 2, no. 2 (2018): 1263–76. https://doi.org/10.31142/ijtsrd9627.

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Space craft to solar system bodies must deal with multiple deviations under the in uence of gravity. The motion of satellite in one of the types of conic section strongly depends upon escape velocity. The goal of this paper is to nd the trajectory of satellite by analysing orbits eccentricity and or bital parameters. This paper also focuses on the derivation of general orbit equation from the base called Newtons law of motion and Newtons law of gravitation. N. Gayathri | S. Mahalakshmi "A Study on Orbital Mechanics" Published in International Journal of Trend in Scientific Research a
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Dwi Aryani, Puput. "Analisis Klasifikasi dan Korelasi Antara Visibilitas Hilal dengan Bujur Perigee dan Apogee Tahun 1300h-1600h." Azimuth: Journal of Islamic Astronomy 6, no. 1 (2025): 79–131. https://doi.org/10.15642/azimuth.v6i1.2672.

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This article analyzes the classification and correlation between the longitudes of perigee and apogee with crescent moon visibility to understand the influence of these factors on the determination of the beginning of the lunar month. Primary data sources were obtained from calculated classifications of crescent moon visibility based on the longitudes of perigee and apogee from the years 1300H to 1600H for three locations: Sabang, Surabaya, and Merauke. Secondary data were sourced from Microsoft Excel. Data collection was conducted through documentation by studying the books Lunar Tables and P
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Maslova, A. I., A. V. Pirozhenko, and O. O. Pirozhenko. "Effect of the solar radiation pressure on the motion of satellites in almost circular Earth orbits." Technical mechanics 2024, no. 2 (2024): 41–54. http://dx.doi.org/10.15407/itm2024.02.041.

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This paper considers the effect of the solar radiation pressure on the motion of a satellite in an almostcircular low-Earth orbit. The formulation of the problem is due to the need to determine the effect of solar radiation pressure forces on the motion of light commercial Earth remote sensing (ERS) satellites with large surface areas (solar batteries and antennas). The goal is to determine the main regularities of this effect, construct reasonably simple and accurate estimates of changes in orbital parameters for the orbits under consideration, and clarify their physics (cause-and-effect rela
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Terekhov, O., R. A. Sunyaev, D. Denisenko та ін. "Observations of γ-ray Bursts and Solar Flares with Granat". International Astronomical Union Colloquium 151 (1995): 353–57. http://dx.doi.org/10.1017/s025292110003534x.

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The Granat observatory was launched into a high apogee orbit on 1989 December 1 by a PROTON launcher. The initial Granat orbit had an apogee close to 200000 km and a perigee of 2000 km with an orbital period of 4 days. The satellite is entering the radiation belts for a few hours every orbit. Due to orbital evolution the perigee increased and the apogee decreased with time. After about 1.5 years of operation the perigee increased up to 20000 km. This has put the satellite completely outside of the proton radiation belts which makes the detector activation during the perigee passage negligible.
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ZHANG, C. M. "QUASI PERIODIC OSCILLATIONS IN X-RAY NEUTRON STAR AND PROBES OF PERIHELION PRECESSION OF GENERAL RELATIVITY." International Journal of Modern Physics D 11, no. 04 (2002): 503–10. http://dx.doi.org/10.1142/s0218271802001822.

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We ascribe the twin kilohertz Quasi Periodic Oscillations (kHz QPOs) of X-ray spectra of Low Mass X-Ray Binaries (LMXBs) to the pseudo-Newtonian Keplerian frequency and the apogee and perigee precession frequency of the same matter in the inner disk, and ascribe 15–60 Hz QPO (HBO) to the apogee (or perigee) precession and its second harmonic frequency to both apogee and perigee precession in the outer disk boundary of the neutron star (NS) magnetosphere. The radii of the inner and outer disks are correlated each other by a factor of two is assumed. The obtained conclusions include: all QPO fre
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Mahdi, Mohammed Chessab. "Study the Space Debris Impact in the Early Stages of the Nano-Satellite Design." Artificial Satellites 51, no. 4 (2016): 163–72. http://dx.doi.org/10.1515/arsa-2016-0014.

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Abstract The probability of KufaSat collisions with different sizes of orbital debris and with other satellites which operating in the same orbit during orbital lifetime was determined. Apogee/Perigee Altitude History was used to graph apogee and perigee altitudes over KufaSat lifetime. The required change in velocity for maneuvers necessary to reentry atmospheric within 25 years was calculated. The prediction of orbital lifetime of KufaSat using orbital parameters and engineering specifications as inputs to the Debris Assessment Software (DAS) was done, it has been verified that the orbital l
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Perryman, M. A. C. "In-Orbit Status of the Hipparcos Astrometry Mission." Symposium - International Astronomical Union 141 (1990): 297–305. http://dx.doi.org/10.1017/s0074180900086976.

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The Hipparcos satellite was successfully launched by Ariane 4 flight 33, from French Guyana, on 8 August 1989. However, the apogee boost motor, designed to place the satellite into its intended geostationary orbit, failed to function, and the satellite was left in a highly elliptical transfer orbit. After a perigee raising manoeuvre, using the hydrazine propulsion system, the orbital parameters are approximately: apogee 35900 km, perigee 526 km, eccentricity 0.72, inclination 6.8°, orbital period 10h 40m.Operational procedures have had to be revised during the first weeks of satellite operatio
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Jeyakodi David, Jim Fletcher, and Ram Krishan Sharma. "Lifetime Estimation of the Upper Stage of GSAT-14 in Geostationary Transfer Orbit." International Scholarly Research Notices 2014 (October 29, 2014): 1–8. http://dx.doi.org/10.1155/2014/864953.

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The combination of atmospheric drag and lunar and solar perturbations in addition to Earth’s oblateness influences the orbital lifetime of an upper stage in geostationary transfer orbit (GTO). These high eccentric orbits undergo fluctuations in both perturbations and velocity and are very sensitive to the initial conditions. The main objective of this paper is to predict the reentry time of the upper stage of the Indian geosynchronous satellite launch vehicle, GSLV-D5, which inserted the satellite GSAT-14 into a GTO on January 05, 2014, with mean perigee and apogee altitudes of 170 km and 3597
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Sinha, A. K., T. K. Yeoman, J. A. Wild, D. M. Wright, S. W. H. Cowley, and A. Balogh. "Evidence of transverse magnetospheric field line oscillations as observed from Cluster and ground magnetometers." Annales Geophysicae 23, no. 3 (2005): 919–29. http://dx.doi.org/10.5194/angeo-23-919-2005.

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Abstract. The dynamic spectrum of ULF waves from magnetic field data obtained by the elliptically orbiting Cluster satellites (with an apogee of 119000km, perigee of 19000km and the orbital period of 57h) have been prepared in the frequency range 0 to 120mHz when the satellite was near its perigee. The existence of field line oscillations, with increasing frequency in the inbound sector and decreasing frequency in the outbound sector, is seen in the transverse components, indicating the presence of independently oscillating local magnetic flux tubes in the form of transverse standing Alfvén wa
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Stoklosa, Adam M., Ilan Weiss, Bruce Bugbee, Michele H. Perchonok, and Lisa J. Mauer. "Composition and Functional Properties of Apogee and Perigee Compared to Common Terrestrial Wheat Cultivars." Habitation 12, no. 1 (2009): 1–8. http://dx.doi.org/10.3727/154296610x12686999887049.

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Dissertations / Theses on the topic "Perigee and Apogee radius"

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Caswell, Joseph M. "THE POTENTIAL ROLE OF CONSCIOUSNESS IN THE COLLAPSE OF RANDOM PHYSICAL SYSTEMS: A QUANTITATIVE BIOPHYSICAL INVESTIGATION OF COGNITIVE INTENTION." Thesis, Laurentian University of Sudbury, 2014. https://zone.biblio.laurentian.ca/dspace/handle/10219/2202.

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Decades of research into the anomalous phenomenon of consciousness-correlated collapse of random systems has supported the contention that human intention appears capable of eliciting significant deviations within these external systems. The following series of experiments was conducted in order to identify potential physical factors which might play a role in the consciousness-correlated effects on a random event generator device. Transcerebral application of a specific physiologically-patterned electromagnetic field was found to enhance the occurrence of this consciousness-mediated interacti
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Books on the topic "Perigee and Apogee radius"

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Mitchell, Eddie. Apogee, perigee, and recovery: Chronology of the Army exploitation of space. Rand, 1991.

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Book chapters on the topic "Perigee and Apogee radius"

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Song, Zhengyu, Cong Wang, and Yong He. "Autonomous Guidance Control for Ascent Flight." In Autonomous Trajectory Planning and Guidance Control for Launch Vehicles. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-0613-0_2.

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AbstractThe purpose of the guidance control is to release a payload into a prescribed target orbit (PTO) accurately. The parameters that determine an orbit are called orbital elements (OEs), which include the semi-major axis a, the eccentricity e, the argument of perigee $$\omega $$ ω , the inclination angle i, and the longitude of ascending node (LAN) or the right ascension of ascending node (RAAN) $$\Omega $$ Ω , where a and e can be converted to the perigee height $$h_p$$ h p and the apogee height $$h_a$$ h a . Thus, the guidance mission of a launcher is a typical optimal control problem with multi-terminal constraints, which requires complex iterative calculations. Considering various constraints in practical applications, such as the accuracy of inertial navigation systems and the performances of embedded computing devices (speed and storage capacity), guidance methods need to balance the mission requirements, hardware resources, and algorithm complexity. A variety of guidance methods has been developed with distinct era characteristics.
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"CHAPTER TWO: Apogee and Perigee of the Bismarck "Dictatorship"." In Bismarck and the Development of Germany, Volume III. Princeton University Press, 1990. http://dx.doi.org/10.1515/9781400861095.31.

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"2 From Apogee to Perigee: Radical Behaviorism Appears but Fails to Take Root." In Control. New York University Press, 2022. http://dx.doi.org/10.18574/nyu/9780814759967.003.0006.

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Conference papers on the topic "Perigee and Apogee radius"

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STECHMAN, R. "Modification of the Space Shuttle primary thruster (870 Lbf) for apogee and perigee kick stages." In 21st Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-1222.

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Ramio-Tomas, Laia, Bertrand Raffier, and Carole Dufour. "SWOT: an AOCS answering to high payload constraints and a controlled reentry of a large satellite." In ESA 12th International Conference on Guidance Navigation and Control and 9th International Conference on Astrodynamics Tools and Techniques. ESA, 2023. http://dx.doi.org/10.5270/esa-gnc-icatt-2023-028.

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Following the successful series of the Jason satellites family, the French-US SWOT (Surface Water and Ocean Topography) satellite was launched at the end of 2022. Thanks to its wide-swath Ka-band radar interferometer, KaRin, developed by the NASA-JPL, it will offer a new opportunity for measuring the surface water height of lakes, river and flood zones, and for seeing mesoscale and sub-mesoscale circulation patterns of oceans. The platform, developed by Thales Alenia Space for CNES, is dimensioned for a satellite mass near 2 tons and a large power supply near 6.6 kWs in order to satisfy the mi
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Santilli, Francesco, Andrew Hyslop, Mariel Triggianese, et al. "The CIMR satellite– challenges and design solutions for AOCS system." In ESA 12th International Conference on Guidance Navigation and Control and 9th International Conference on Astrodynamics Tools and Techniques. ESA, 2023. http://dx.doi.org/10.5270/esa-gnc-icatt-2023-177.

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The Copernicus Imaging Microwave Radiometer (CIMR) is a European Earth Observation mission consisting of 2 satellites (with an option of the extension to the third one). It will provide high resolution global monitoring of the Earth surface emissions across various frequency bands, in particular floating sea ice parameters. The 3-axis stabilized spacecraft(s) will operate in a sun synchronous orbit with 817 km altitude. The instrument features a deployable mesh reflector with the diameter of 8 meters and its feed cluster, which rotates at 8 rpm to produce a 1900km wide ground swath. The CIMR m
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Bonaccorsi, Sergio, Marco Felice Montaruli, Pierluigi Di Lizia, et al. "A software suite for conjunction analysis assessment in Space Surveillance and Tracking applications." In ESA 12th International Conference on Guidance Navigation and Control and 9th International Conference on Astrodynamics Tools and Techniques. ESA, 2023. http://dx.doi.org/10.5270/esa-gnc-icatt-2023-123.

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In the last decades, the growing in-orbit population of resident objects has become one of the main concerns for space agencies and institutions worldwide, and several Space Surveillance and Tracking (SST) related initiatives have been promoted to tackle this issue. Indeed, the presence of the so-called space debris may jeopardise the operative mission of active satellites, given that the possible impact with a space debris ranges from cumulative erosion of satellite surface to the possible satellite destruction, with the generation of thousands of additional pieces of debris and inevitable en
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