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Operational Experience with X-15 Reaction Controls
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English
Abstract
The four reaction control system configurations investigated during the X-15 program include a proportional acceleration command system, on-off proportional rate command and attitude hold systems, and a rate sensing on-off stability augmentation system. Each of the systems is described briefly, and development problems encountered in hardware design, component compatibility, and systems integration are discussed. The practical aspects of system design and operation are emphasized.
Flight experience with each system is also discussed. Flight data showing the results of open-loop and closed-loop control during critical X-15 reentry maneuvers are presented.
Authors
Citation
Jarvis, C. and Adkins, E., "Operational Experience with X-15 Reaction Controls," SAE Technical Paper 640246, 1964, https://doi.org/10.4271/640246.Also In
References
- Holleman, Euclid C. Stillwell, Wendell H. “Simulator Investigation of Command Reaction Controls.” NACA 1958
- Love, James E. Stillwell, Wendell H. “The Hydrogen-Peroxide Rocket Reaction-Control System for the X-1B Research Airplane.” NASA 1959
- Reisert, Donald Adkins, Elmor J. “Flight and Operational Experiences With Pilot Operated Reaction Controls.” ARS Jour. 32 April 1962 626 631
- Cooper, George E. “Understanding and Interpreting Pilot Opinion.” Aero. Eng. Rev. 16 March 1957 47 51 56