The difficulty encountered in operating a final-value control system in a closed-loop configuration is that the feedback gains become infinite at the final time and thus are impossible to implement. This thesis examines several alternative configurations to the closed-loop system for the Titan III booster using Flight Plan I pitch steering. (Author)
A Study in Final-Value Control
1970
107 pages
Report
Keine Angabe
Englisch
Control Systems & Control Theory , Spacecraft Trajectories & Flight Mechanics , Launch vehicles(Aerospace) , Adaptive control systems , Flight control systems , Mathematical models , Differential equations , Feedback , Theses , Titan 3 , Closed loop control systems , Feedback control , Control theory
Stochastic final value control
AIAA | 1968
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