期刊
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
卷 22, 期 6, 页码 2103-2117出版社
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TCST.2014.2303787
关键词
Aircraft Navigation; motion planning; nonlinear control systems; unmanned systems
资金
- Division Of Computer and Network Systems
- Direct For Computer & Info Scie & Enginr [1161036] Funding Source: National Science Foundation
This paper considers the problem of fixed wing unmanned air vehicles following straight lines and orbits. To account for ambient winds, we use a path following approach as opposed to trajectory tracking. The unique feature of this paper is that we explicitly account for roll and flight path angle constraints. The guidance laws are derived using the theory of nested saturations, and explicit flight conditions are derived that guarantee convergence to the path. The method is validated by simulation and flight tests.
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