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3DOF ascent phase trajectory optimization for aircraft based on adaptive Gauss Pseudospectral Method

机译:基于自适应高斯伪谱方法的飞机三自由度上升阶段轨迹优化

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3DOF ascent phase trajectory optimization problem for minimum fuel-to-climb is investigated in the research. The Gauss Pseudospectral Method (GPM) and adaptive strategy is proposed to transcribe the trajectory optimization problem into a Nonlinear Program Problem (NLP). Then, the Sequential Quadratic Programming (SQP) integrated in a sparse nonlinear program solver named SNOPT is used to solve the resulting NLP problem with a proper initial guess. The optimality of the ascent trajectory is also checked via Bellman's principle. The simulation results demonstrate that the method can generate a feasible 3DOF ascent trajectory with all constraints satisfied.
机译:在研究中,研究了最小自由度爬升的3DOF上升阶段轨迹优化问题。提出了高斯伪谱方法(GPM)和自适应策略,将轨迹优化问题转化为非线性程序问题(NLP)。然后,将集成在稀疏非线性程序求解器SNOPT中的顺序二次规划(SQP)用于通过适当的初始猜测来解决由此产生的NLP问题。还通过Bellman原理检查上升轨迹的最优性。仿真结果表明,该方法可以在满足所有约束条件的情况下,生成可行的3DOF上升轨迹。

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