Paper derives and analyzes method of steering rocket vehicle so as to achieve ballistic trajectory that arrives at specific position at specific time; result contained is substantial refinement of fly-by-wire method for exoatmospheric steering; simulation results show that since steering equation is sufficiently accurate, no trajectory-dependent preflight calculations need be done when simple in-flight choice of certain constants is made.
Steering law satisfying constant total time of flight constraint
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 4 , n 11
1967
5 pages
Article (Journal)
English
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