Improving Control Allocation Accuracy for Nonlinear Aircraft Dynamics-Reference-Cited by-同舟云学术

Improving Control Allocation Accuracy for Nonlinear Aircraft Dynamics

Published:2002-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
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Author:

Doman David¹,Oppenheimer Michael²

Affiliation:

1. Air Force Research Laboratory

2. Veridian Engineering

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4667

Reference8 articles.

1. "Application of Multivariable Control Theory to Aircraft Control Laws," Tech. Rep. WLTR-96-3099, USAF Wright Laboratory, WrightPattersonAFB,OH,May1996. INNER LOOP

2. Evaluation of optimization methods for control allocation

3. 5 10 15 20 25 30 -60 Dashed Line: Flight-Path Angle without ε(P,δ) Dashed Line: Flight-Path Angle without ε(P,δ)

4. Dynamic Inversion-Based Adaptive/Reconfigurable Control of the X-33 on Ascent

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