Nonlinear Analysis for Wing-Rock System with Adaptive Control
Author:
Affiliation:
1. Nanjing University of Science and Technology, 210094 Nanjing, People’s Republic of China
2. Cranfield University, Cranfield, England MK43 0AL, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G006775
Reference28 articles.
1. Output Feedback Adaptive Control of Plants with Unmodeled Dynamics and Input Uncertainties
2. Experimental Validation of L1 Adaptive Control: The Rohrs Counterexample in Flight
3. Time-Delay Margin Analysis for an Adaptive Controller
4. Optimisation-Based Clearance
5. Application of bifurcation methods to nonlinear flight dynamics problems
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