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L1 Adaptive Control with Switched Reference Models: Application to Learn-to-FlyLearn-to-Fly (L2F) is a new framework that aims to replace the traditional iterative development paradigm for aerial vehicles with a combination of real-time aerodynamic modeling, guidance, and learning control. To ensure safe learning of the vehicle dynamics on the fly, this paper presents an L1 adaptive control (L1AC) based scheme, which actively estimates and compensates for the discrepancy between the intermediately learned dynamics and the actual dynamics. First, to incorporate the periodic update of the learned model within the L2F framework, this paper extends the L1AC architecture to handle a switched reference system subject to unknown time-varying parameters and disturbances. The paper also includes analysis of both transient and steady-state performance of the L1AC architecture in the presence of non-zero initialization error for the state predictor. Second, the paper presents how the proposed L1AC scheme is integrated into the L2F framework, including its interaction with the baseline controller and the real-time modeling module. Finally, flight tests on an unmanned aerial vehicle (UAV) validate the efficacy of the proposed control and learning scheme.
Document ID
20210017601
Acquisition Source
Langley Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Steven Snyder ORCID
(Langley Research Center Hampton, Virginia, United States)
Pan Zhao
(University of Illinois at Urbana Champaign Urbana, Illinois, United States)
Naira Hovakimyan
(University of Illinois at Urbana Champaign Urbana, Illinois, United States)
Date Acquired
June 16, 2021
Publication Date
August 17, 2022
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Publisher: American Institute of Aeronautics and Astronautics
Volume: 45
Issue: 12
Issue Publication Date: December 1, 2022
ISSN: 0731-5090
e-ISSN: 1533-3884
Subject Category
Air Transportation And Safety
Aircraft Stability And Control
Aircraft Communications And Navigation
Funding Number(s)
WBS: 109492.02.07.05.05
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
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