NASA NTRS · 19920035215
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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Cheng, Peter Y., Chan, Samuel Y., Myers, Thomas T., Klyde, David H., Mcrue, Duane T.. 1991-12-01. Aeroservoelastic stabilization techniques for hypersonic flight vehicles. https://ntrs.nasa.gov/citations/19920035215
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