Control scheme to minimize lateral drift and concurrently to maintain structural load limits of vehicle is presented and compared with conventional vehicle attitude control schemes; guidance problem is solved by directing acceleration vector in manner that will cause vehicle to move from its present state to desired future state; conventional vehicle attitude control schemes insure stable rotational dynamic behavior of vehicle by attempting to bring its attitude into coincidence with desired attitude; it also is independent of vehicle attitude feedback.
Acceleration vector attitude control system
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 5 , n 6
1968
6 pages
Article (Journal)
English
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An acceleration vector attitude control system.
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