Relevant bibliographies by topics / Rocket steering

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  2. Book chapters
  3. Conference papers

Academic literature on the topic 'Rocket steering'

Author: Grafiati
Published: 3 June 2025
Last updated: 31 July 2025

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Journal articles on the topic "Rocket steering"

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Anand, R. "Computational steady-thrust vector controlsupersonic secondary flow injection." Aeronautics and Aerospace Open Access Journal 5, no. 1 (2021): 33–36. http://dx.doi.org/10.15406/aaoaj.2021.05.00125.

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This paper presents the Computational study of flow through the Rocket Nozzle in order to manoeuvre the Rocket by means of Supersonic Secondary Injection of Hot gases. Well-designed nozzles can accelerate these gases to speeds of thousands of meters per second. In addition to accelerating the gases, nozzles are often responsible for steering (or “vectoring”) the flow in order to control the rocket’s direction of flight. Due to continuous secondary injection of hot gases, the strong unsteady effects like Shear Layers, Intervention of Shockwaves with the Core fluid flow, Biased Wall Shear, etc.,
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Mandić, S. "Dispersion reduction of artillery rockets guided by flight path steering method." Aeronautical Journal 120, no. 1225 (2016): 435–56. http://dx.doi.org/10.1017/aer.2016.4.

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ABSTRACTArtillery rockets are sensitive to disturbances (total impulse variation, wind, thrust misalignment, etc.). As the range of ground-to-ground rockets increases, the accuracy of free flight rockets decreases. Requirements for the increase of the range and minimisation of the impact point dispersions can be solved by adding guidance and control systems to rockets. Based on the differences between the measured flight parameters and the calculated parameters for the nominal trajectory, the flight path angle correction algorithm is obtained by adding the correction to the nominal value. The
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Belonogov, O. B. "Investigation of the Influence of Structural and Adjusting Parameters of a Quadruple-Orifices Electrohydraulic Amplifier on the Static Characteristics of Rocket Pack Steering Actuator." Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, no. 6 (129) (December 2019): 32–40. http://dx.doi.org/10.18698/0236-3941-2019-6-32-40.

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The article considered the results of researches of influence of constructional and adjusting parameters of the quadruple-orifices electrohydraulic amplifier on static characteristics of the steering actuator of the rocket pack. The studies are carried out using static analysis methods, including methods for calculating the static characteristics of an autonomous single-stage steering actuator with a quadruple-orifices electrohydraulic amplifier with negative overlapping of throttling windows of rectangular shape by spool plungers. As a result of research it is shown that the steering actuator
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Tokareva, Olena Leonidivna, Natalia Serhiivna Priadko, and Ternova Vitaliivna Ternova. "An operation algorithm for the combined thrust vector control system of a rocket engine." System technologies 4, no. 123 (2019): 58–66. http://dx.doi.org/10.34185/1562-9945-4-123-2019-06.

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The new combined rocket engine (RE) control system consists of combining various control systems - mechanical thrust vector control system (MTVCS) and gas-dynamic one (GDTVCS) within one bifunctional system that performs the functions of controlling and stabilizing the rocket stage flight. Previously it was shown that the MTVCS speed has limit, since with its speed increase the sensitivity to high-frequency random disturbances rises, which increases random errors. In addition, the system performance rise leads to an increase in the mass and dimensions of the steering drive of the engine swing.
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Zaytsev, Nikolay, Andrey Bondarenko, and Dmitriy Pyankov. "SIMULATION OF DYNAMICS OF THE SWIVEL CONTROL NOZZLE WITH DOUBLE ELASTIC JOINT." Perm National Research Polytechnic University Aerospace Engineering Bulletin, no. 60 (2020): 34–44. http://dx.doi.org/10.15593/2224-9982/2020.60.04.

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In order to create control moments for the rocket, the design of modern solid propellant rocket engines uses swivel control nozzles with elastic support joint. The disadvantage of such a joint as the nozzle suspension is the high joint torque, which determines the high requirements for power and effort of steering actuators. In order to reduce these requirements, it is possible to use the design of a swivel control nozzle with a double elastic joint, known as a nozzle with double elastic seal. This nozzle is not used due to its design and operational complexity, particularly due to its tendenc
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Timarov, A. G., A. N. Efremov, and R. V. Bulbovich. "Numerical simulation of jet vane carry-over effect on steering effort." Journal of «Almaz – Antey» Air and Space Defence Corporation, no. 3 (September 30, 2016): 47–51. http://dx.doi.org/10.38013/2542-0542-2016-3-47-51.

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By using advanced computational tools, we developed an engineering design procedure to determine the steering effort generated due to the deviation of the jet vane in the solid engine. In addition to testing the calculation data, the aim of this study is to have an opportunity of a more detailed examination of the jet vane effect on the flow in a rocket engine, followed by visualization of the processes.
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Smith, John Maynard. "Explanation in Biology: Explanation in Biology." Royal Institute of Philosophy Supplement 27 (March 1990): 65–72. http://dx.doi.org/10.1017/s135824610000504x.

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During the war, I worked in aircraft design. About a year after D-day, an exhibition was arranged at Farnborough of the mass of German equipment that had been captured, including the doodlebug and the V2 rocket. I and a friend spent a fascinating two days wandering round the exhibits. The questions that kept arising were ‘Why did they make it like that?’, or, equivalently ‘I wonder what that is for?’ We were particularly puzzled by a gyroscope in the control system of the V2. One's first assumption was that the gyroscope maintained the rocket on its course, but, instead of being connected to t
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Timarov, Aleksey, Andrey Efremov, and Roman Bulbovich. "SOME ISSUES OF CALCULATION OF STEERING EFFORTS OF ROCKET MOTOR JET VANES." Perm National Research Polytechnic University Aerospace Engineering Bulletin, no. 48 (2017): 35–42. http://dx.doi.org/10.15593/2224-9982/2017.48.04.

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Dvornychenko, V. N. "Optimal rocket steering in terms of angular velocity of the primer vector." Journal of Guidance, Control, and Dynamics 16, no. 6 (1993): 1188–91. http://dx.doi.org/10.2514/3.21148.

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Buchanan, C. R., A. J. T. Gemmill, and P. G. Martin. "Interaction of missile propulsion and aerodynamics." Aeronautical Journal 104, no. 1036 (2000): 271–77. http://dx.doi.org/10.1017/s0001924000091594.

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Abstract Some aspects of propulsion integration issues for ramjet powered missiles are outlined in this paper. The benefits of ramjet propulsion in the Mach 2-4 range over other types of airbreathing propulsion and rocket propulsion are well known. Compared with solid rocket motors, ramjet engines offer a much higher specific impulse and the capability of thrust management, enabling longer stand-off ranges and more flexible operation. An overview of the ramjet engine cycle is given, highlighting engine/intake matching issues. This is followed by a performance comparison between a generic ramje
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Book chapters on the topic "Rocket steering"

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Domning, Daryl P. "The Terrestrial Posture of Desmostylians." In Smithsonian Contributions to Paleobiology. Smithsonian Institution Press, 2002. http://dx.doi.org/10.5479/si.00810266.93.99.

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An attempt to reconstruct a skeleton of <i>Paleoparadoxia </i>Reinhart, 1959 (Mammalia, Desmostylia), suggests that desmostylian terrestrial posture deviated from that of typical ungulates much less than has been supposed by other authors. Desmostylians probably had a quadrupedal stance, with the body welt off the ground and the limbs more or less under the body; a strongly arched spine and steeply inclined pelvis; slightly abducted elbows and more strongly abducted knees; and a digitigrade foot posture with an extended but not hyperextended wrist and hyperextended toes, the front
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Lorbiecki, Marybeth. "The Wilderness Idea." In A Fierce Green Fire. Oxford University Press, 2016. http://dx.doi.org/10.1093/oso/9780199965038.003.0024.

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It was supposed to be a day of short, easy paddles and portages. But that is before the winds show up, gale force and pummeling wave after wave against us, determined to lock us down on the island. We pull our three canoes laden with children and camping gear along the edges of the rocky shore to try to find an easier launching point. The teens then take steering positions, as we throw our shoulders into our paddles and dig, over, and over into those icy blasts of heavy, strong-armed water. Any lapse sends the canoe back. One slip of weight, and we’ll tip, losing all our gear, and we’ll have t
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Conference papers on the topic "Rocket steering"

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Scharring, Stefan, Daniela Hoffmann, Hans-Albert Eckel, et al. "Remotely Controlled Steering Gear For A Laser-Driven Rocket With A Parabolic Thruster." In BEAMED ENERGY PROPULSION: 6th International Symposium. AIP, 2010. http://dx.doi.org/10.1063/1.3435461.

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De Oliveira, Alice, and Michèle Lavagna. "Robust Control Design via Structured H-infinity for the Atmospheric Re-entry of Reusable Launchers." 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-2023-191.

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The controlled atmospheric re-entry associated with the precision soft-landing of Reusable Launch Vehicles (RLVs) on Earth is very challenging as it depends on multiple parameters [1]. Over the last decade, the cost-effectiveness of such a technology has been finally demonstrated with the successful recoveries of SpaceX’s Falcon 9 first-stage rocket first [2], then followed by other companies such as the Rocket Lab’s Electron micro-launcher [3]. This breakthrough has been made possible by the development of advanced and robust computational methods able to generate in real time the flight cond
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Saravanan, Om, Mamatha J, Chandana C, Sukanthraj R, and Lakshmi K. "Self-balancing E-bike." In International Conference on Recent Trends in Computing & Communication Technologies (ICRCCT’2K24). International Journal of Advanced Trends in Engineering and Management, 2024. http://dx.doi.org/10.59544/zhsz6075/icrcct24p90.

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Today, automation is essential rather than optional, especially as two wheeler accidents continue to occur despite various safety precautions. Many of these incidents result from loss of balance or control. Customers are increasingly demanding self balancing systems for two wheelers to address this issue. This paper explores the use of the gyroscopic method to create a self balancing bike. The gyroscopic effect, long employed in stabilizing systems across fields like military rocket guidance, aerospace, aeronautics, and marine navigation, has proven effective over the years. We adapted this pr
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Correa, Adriana Elysa Alimandro, Alex da Rosa, Henrique Cezar Ferreira, Joao Yoshiyuki Ishihara, Renato Alves Borges, and Yuri Dmitrievich Sheptun. "Robust steering control of spacecraft carrier rockets." In 2013 IEEE Aerospace Conference. IEEE, 2013. http://dx.doi.org/10.1109/aero.2013.6497345.

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Franzè, Renato. "Guidance, navigation and control for the autonomous return-to-launch-site functionality of experimental free-falling-units ejected at high altitude from a sounding rocket." 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-2023-077.

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Sounding rockets have been a fundamental component of scientific research related to the near-Earth environment. Free-falling units are ejected from high altitudes in order to perform measurements in different regions of the atmosphere and ionosphere. These units perform reentry by deploying a parachute, thus requiring significant time and resources in order to be retrieved, and the recovery operations often happen to be unsuccessful. The BOOMERANG team from the REXUS/BEXUS programme is aiming to address this problem by developing an autonomous return-to-launch-site functionality that can be m
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Chen, T., G. H. Liu, X. He, and J. Li. "Analysis of Factors Influencing the Deflection Capacity of the Internal Push Point-The-Bit Rotary Steering Tool." In 57th U.S. Rock Mechanics/Geomechanics Symposium. ARMA, 2023. http://dx.doi.org/10.56952/arma-2023-0057.

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ABSTRACT The internal push point-the-bit rotary steering tool is a new type of dynamic point-the-bit rotary steerable system. Deflection capacity is an important index to measure the performance of rotary steering tools. To study the influencing factors of deflection capacity, it is necessary to clarify the variation law of build-up rate with each influencing factor, which can provide a basis for tool design optimization and drilling process design. Based on the calculation model of the build-up rate of the internal push point-the-bit rotary steering tool, this paper analyzes the influence of
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Xu, Guoyan, Xiaopo Wang, Feng Gao, Xiaolin Xie, and Nenggen Ding. "Design and Structure Analysis of Wheeled Chassis With Self-Balancing Rocker of Rescue Engineering Machinery." In ASME 2013 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/imece2013-63568.

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A wheeled chassis with self-balancing rocker is developed for rescue engineering machinery. This chassis has better ground adaptability compared with traditional ones because of the automatically adjustable ground clearance and body posture, non-trapezium steering mechanism, independent four-wheel steering, and “X”-type radiation legs. Finite element analysis on the chassis structure is done with two mechanical models and under typical finite element working conditions. HyperWorks software is used to analyze different parts of the chassis, and the results are used for structure optimization. T
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Liu, Kerou, Hui Zhang, Renjun Xie, et al. "New Steering Technology Using Pulsed Arc Plasma Shockwave: Plasma Pulse Steering Technology." In SPE Middle East Oil & Gas Show and Conference. SPE, 2021. http://dx.doi.org/10.2118/204868-ms.

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Abstract Steering drilling technology can achieve precise control of wellbore trajectory, and related technologies have been widely used in the field of petroleum drilling. This paper proposed a new steering drilling technology based on the Pulsed Arc Plasma Shockwave Technology (PAPST),Plasma Pulse Steering Technology (PPST). PAPST transforms electric energy into mechanical energy by discharging electrodes, which can break rock. On the basis of PAPST, PPST can precisely control the discharge time and break the rock in the specified direction at the bottom of the well, so as to realize guided
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Jørgensen, Ole. "Using Flow Induced Stresses for Steering of Injection Fractures." In SPE/ISRM Rock Mechanics Conference. Society of Petroleum Engineers, 2002. http://dx.doi.org/10.2118/78220-ms.

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Oe, Asahi, Shin-Ichiro Nishida, and Shintaro Nakatani. "Study of Passive Steering Mechanism for Mars Surface Exploration Rovers." In 11th Asia-Pacific Regional Conference of the ISTVS. International Society for Terrain-Vehicle Systems, 2022. http://dx.doi.org/10.56884/rdkv9886.

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In planetary exploration, rovers are used to move across the surface to obtain high-resolution topographic elevation maps, as well as to conduct mining and rock sampling. However, because of the harsh planetary environment, surface exploration poses many technical challenges. In this study, we assume an unmanned exploration rover that is small enough to be carried on a Japanese launch vehicle, and its weight is limited by the payload capacity of the launch vehicle. It is also important that the rover is not prone to failure. The surface of Mars is covered with fine sand called regolith, and th
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