NASA NTRS · 19910020842
Aeroservoelastic stabilization techniques for hypersonic flight vehicles
Abstract
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.
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Chan, Samuel Y., Cheng, Peter Y., Pitt, Dale M., Myers, Thomas T., Klyde, David H., Magdaleno, Raymond E., Mcruer, Duane T.. 1991-09-01. Aeroservoelastic stabilization techniques for hypersonic flight vehicles. https://ntrs.nasa.gov/citations/19910020842
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