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Flight control design using non-linear inverse dynamics

✍ Scribed by Stephen H. Lane; Robert F. Stengel


Publisher
Elsevier Science
Year
1988
Tongue
English
Weight
832 KB
Volume
24
Category
Article
ISSN
0005-1098

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Adaptive flight control using optimal li
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An adaptive control system, developed using regulator theory and applied to the lateral equations of motion for an aircraft, utilizes components which include estimation logic and a model following control law. Summary--Simple mechanical linkages are often unable to cope with the many control probl