Optimal Nonlinear Feedback Guidance for Reentry Vehicles-Reference-Cited by-同舟云学术

Optimal Nonlinear Feedback Guidance for Reentry Vehicles

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
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Author:

Bollino Kevin¹,Ross Michael¹,Doman David²

Affiliation:

1. Naval Postgraduate School

2. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6074

Reference28 articles.

1. Reconfigurable Control Design for the X-40A with In-Flight Simulation Results

2. Reconfigurable Inner Loop Control of a Space Maneuvering Vehicle

3. Nonlinear Control Allocation Using Piecewise Linear Functions

4. 5Doman,D.B.,andOppenheimer,M.W."IntegratedAdaptiveGuidanceandControlforSpaceAccessVehicles, Volume 1: Reconfigurable Control Law for X-40A Approach and Landing," AFRL IAG&C Technical Report, Wright-PattersonAFB,OH,2004.

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