Optimal target aiming maneuver for an advanced aircraft via timescale pseudospectral method
Liao Kaijun, Qian Kun, Hao Yan, Qian Zhengzai, Sun Yuqian
Abstract
Liao Kaijun, Qian Kun, Hao Yan, Qian Zhengzai, Sun Yuqian
Abstract
A two-timescale Chebyshev pseudospectral optimal control method, which can reduce the converted nonlinear programming (NLP) significantly, is proposed. The optimal aiming maneuver problem of an advanced aircraft, which is a six-degree-of-freedom trajectory problem, is solved by this two-timescale method. It is the first time that the six-degree-of-freedom equations are used to solve optimization of the flight trajectory problems.
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A two-timescale Chebyshev pseudospectral optimal control method, which can reduce the converted nonlinear programming (NLP) significantly, is proposed. The optimal aiming maneuver problem of an advanced aircraft, which is a six-degree-of-freedom trajectory problem, is solved by this two-timescale method. It is the first time that the six-degree-of-freedom equations are used to solve optimization of the flight trajectory problems.
Key concepts: Pseudospectral optimal control, Trajectory, Gauss pseudospectral method, Trajectory optimization, Chebyshev pseudospectral method, Pseudo-spectral method, Control theory (sociology), Optimal control