Influence of high-order dynamics on helicopter flight-control systembandwidth
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
2. Stanford University, Stanford, California
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
http://arc.aiaa.org/doi/pdf/10.2514/3.20089
Reference11 articles.
1. A Method for Improving the Inherent Stability and Control Characteristics of Helicopters
2. Inclusion of Rotor Dynamics in Controller Design for Helicopters
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2. Reduced-Order Static L2-Gain Control of Rotorcraft with Guaranteed Rotor–Fuselage Stability;Journal of Guidance, Control, and Dynamics;2023-09
3. Analytical Investigation of the Influence of Rotor Flap Dynamics on Helicopter Flight Control System Feedback Gain Limit;Journal of the Korean Society for Aeronautical & Space Sciences;2020-03-31
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