DocumentCode :
3019103
Title :
Guidance and control of maneuvering reentry vehicles
Author :
Page, J.A. ; Rogers, R.O.
Author_Institution :
The Aerospace Corporation, El Segundo, California
fYear :
1977
fDate :
7-9 Dec. 1977
Firstpage :
659
Lastpage :
664
Abstract :
Over the past fifteen years, studies and flight tests have brought maneuvering reentry technology to a state of relative maturity. During this period, many vehicle configurations have been investigated and many guidance or steering schemes proposed. This paper is intended to summarize those investigations, few of which have been made available to the technic??al community at large. Three vehicle control configurations (cruciform, bank-to-turn, and fixed trim) and three guidance laws (cross-product, proportional, and tangent cubic) are presented in this paper. Each law is formulated for use with each vehicle configuration. The relative merits and drawbacks of these configurations are discussed.
Keywords :
Actuators; Aerodynamics; Aerospace control; Aerospace testing; Control systems; Dynamic range; Force control; Instruments; Navigation; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control including the 16th Symposium on Adaptive Processes and A Special Symposium on Fuzzy Set Theory and Applications, 1977 IEEE Conference on
Conference_Location :
New Orleans, LA, USA
Type :
conf
DOI :
10.1109/CDC.1977.271654
Filename :
4045924
Link To Document :
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