Study is intentionally limited to single control variable case in order to introduce nature of problems encountered in meaningful manner; illustrative examples are used to expose basic analytical difficulties and demonstrate that these are not unsurmountable; it is shown that basic tools of linear optimal control, such as root-square locus, continue to be of great value in uncertain parameter case; resultant theory is applied to design of compensating network required for flexible booster when value for slope of first bending mode is uncertain.
Suboptimal approach to control of systems containing uncertain parameters
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 4 , n 11
1967
7 pages
Article (Journal)
English
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