Real-Time Closed-Loop System Identification of a Quadcopter-Reference-Cited by-同舟云学术

Real-Time Closed-Loop System Identification of a Quadcopter

Published:2019-01 Issue:1 Volume:56 Page:324-335
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Alabsi Mohammed I.¹,Fields Travis D.¹

Affiliation:

1. University of Missouri–Kansas City, Kansas City, Missouri 64110

Funder

NASA EPSCoR

University of Missouri Research Board

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034219

Reference21 articles.

1. Flight Dynamics and Hybrid Adaptive Control of Damaged Aircraft

2. Active fault-tolerant control system against partial actuator failures

3. KoehlerR.WilhelmK. “Closed Loop Aspects of Aircraft Identification. Parameter Identification,” AGARD LS104, Neuilly sur Seine, France, Oct.–Nov. 1979, Paper 10.

4. Aerodynamic parameter estimation from flight data applying extended and unscented Kalman filter

5. Concurrent Learning for Improved Convergence in Adaptive Flight Control

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