Overview

The potential of Hybrid Phase Stabilization (HPS), particularly for highly unstable aircraft, using a hypersonic flight vehicle (HSV) as a relevant example, is discussed. The development of HPS is presented and the result is compared with that generated using a conventional gain stabilization technique. Since HPS was not addressed in the MIL-spec requirements, a preliminary residual response metric was developed to provide guidance in assessing HPS. Chan, Samuel Y. and Cheng, Peter Y. and Pitt, Dale M. and Myers, Thomas T. and Klyde, David H. and Magdaleno, Raymond E. and Mcruer, Duane T. Unspecified Center AEROELASTICITY; AEROSERVOELASTICITY; FLEXIBLE BODIES; FLIGHT CONTROL; HYPERSONIC VEHICLES; STABILIZATION; HYPERSONICS; TIME LAG...

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9781722930905

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