Experimental optimal relay guidance system to control bang-bang, line of sight guidance missile is described; it makes use of both instantaneous pilot commands and past history of commands in order to derive missile maneuver orders which are based on more optimal strategy; proper error nulling is aided by injecting anticipatory synthetic missile dynamics which tend to damp out phase lags and other interactions associated with human and missile aerodynamics.
Optimal bang-bang guidance system
WESCON Convention Rec
WESCON Convention Record ; 6 , Part 5
1962
9 pages
Article (Journal)
English
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Kinematic Constraint and Bang-Bang Guidance Based Performance Enhancement
British Library Conference Proceedings | 2010
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