Minimax studies
Effect of nonzero initial conditions on selection of minimax controllers for large launch vehicles and extremal bounded amplitude bounded rate inputs to linear systems
CONTROL SYSTEM↗
Engineering topics
Graham, K. D.
Publications and source records attributed to Graham, K. D..
Minimax control of large launch boosters
Optimal control theory applied to piecewise constant approximation of large launch booster for first 84 seconds of flight
OPTIMAL CONTROL↗