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• W2083161180 abstract "Ascent phase minimum time-to-climb trajectory optimization problem(TOP) is studied in the paper. To avoid the drawback of indirect methods and traditional direct methods, a new optimal control method-Gauss Pseudospectral Method(GPM) was used to transform the trajectory optimization problem into Nonlinear Program(NLP) problem. A initial guess strategy was proposed to improve the convergence rate of NLP problem, based on the guess, which can be solved using a sparse nonlinear optimization software named SNOPT. The optimality of the solution was verified via checking up the Hamiltonian function. Finally, simulation results demonstrate the efficiency of the method." @default.
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• W2083161180 date "2010-05-01" @default.
• W2083161180 modified "2023-09-25" @default.
• W2083161180 title "Ascent phase trajectory optimization for aircraft based on Nonlinear Programming" @default.
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• W2083161180 doi "https://doi.org/10.1109/ccdc.2010.5498867" @default.
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