Fault-Tolerant Flight Control Using One Aerodynamic Control Surface

Author:

Venkataraman Raghu1,Seiler Peter1

Affiliation:

1. University of Minnesota, Minneapolis, Minnesota 55455

Funder

College of Science and Engineering, University of Minnesota

Division of Computer and Network Systems

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

Reference49 articles.

1. FreemanP. “Reliability Assessment for Low-Cost Unmanned Aerial Vehicles,” Ph.D. Thesis, Univ. of Minnesota, Minneapolis, MN, 2014.

2. Robust Model-Based Fault Diagnosis for Dynamic Systems

3. Fault-Diagnosis Systems

4. Data-driven Design of Fault Diagnosis and Fault-tolerant Control Systems

5. Diagnosis and Fault-Tolerant Control

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3. Data-driven fault-tolerant control for unmanned aerial vehicles without using identification model;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-04-18

4. Dynamics and adaptive fault-tolerant flight control under structure damage of horizontal stabilizer;Aerospace Science and Technology;2020-11

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