Adaptive Flight Control in the Presence of Limits on Magnitude and Rate-Reference-Cited by-同舟云学术

Adaptive Flight Control in the Presence of Limits on Magnitude and Rate

Published:2022 Issue: Volume:10 Page:65685-65702
ISSN:2169-3536
Container-title:IEEE Access
language:
Short-container-title:IEEE Access

Author:

Gaudio Joseph E.¹^ORCID,Annaswamy Anuradha M.¹^ORCID,Bolender Michael A.²,Lavretsky Eugene³^ORCID

Affiliation:

1. Department of Mechanical Engineering, Massachusetts Institute of Technology, Cambridge, MA, USA

2. Air Force Research Laboratory, Wright-Patterson AFB, OH, USA

3. The Boeing Company, Huntington Beach, CA, USA

Funder

Air Force Research Laboratory, Collaborative Research and Development for Innovative Aerospace Leadership (CRDInAL), Thrust 3 - Control Automation and Mechanization

Boeing Strategic University Initiative; cleared for release

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

General Engineering,General Materials Science,General Computer Science,Electrical and Electronic Engineering

Link

http://xplorestaging.ieee.org/ielx7/6287639/9668973/09800767.pdf?arnumber=9800767

Reference54 articles.

1. Sequential Loop Closure Based Adaptive Output Feedback

2. Adaptive Output Feedback Based on Closed-Loop Reference Models for Hypersonic Vehicles

3. An Adaptive Controller for Very Flexible Aircraft

4. Fast learning and adaptation in control and machine learning;gaudio,2020

5. Adaptive Control of Hypersonic Vehicles in the Presence of Rate Limits

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