作者: Fanlin Zeng , Jigong Li , Junfang Li
DOI: 10.1109/ICMA.2015.7237801
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摘要: In this paper we consider nonlinear control of high-speed unmanned aerial vehicle with strong coupling effects. The between aerodynamics, flexible structure and propulsion system will bring great challenges for longitudinal model control. order to overcome the unstable zero dynamics which caused by couplings, an auxiliary plant is constructed purpose feedback design. Then, a decoupling controller designed. reference tracking velocity altitude can be achieved. Simulation results using include intricate couplings engine flight are presented illustrate effectiveness proposed method.