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Optimization of projectile state and trajectory of reentry body based on Hp-adaptive pseudospectral method

机译:基于Hp的伪谱方法优化弹丸状态和再入弹道

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Considering the path constraints, control constraints and initial/terminal states constraints, optimal projectile state and trajectory of reentry body are designed based on hp-adaptive pseudospectral method to achieve maximum range. Path constraints include normal overload constraint, dynamic pressure constraint and heating rate constraint; control constraints include angle of attack constraint and bank angle constraint; initial/terminal states constraints include altitude constraint, velocity constraint and flight path angle constraint. In face of the fact that the range of optimal control solution resulted from pseudospectral method may be unsmooth, virtual control variables (second derivatives of the angle of attack and bank angle) are proposed in the optimization, while the angle of attack and bank angle are treated as the virtual state variables to guarantee the smoothness of the optimal control solution. The validity of hp-adaptive pseudospectral method in dealing with nonlinear, multi-constrained, multi-variable optimization problems is verified by simulation, and the consistency between the solution obtained and the first-order necessary conditions for optimality of indirect method is confirmed using the costate and Hamiltonian.
机译:考虑到路径约束,控制约束和初始/终态约束,基于hp自适应伪谱方法设计了最佳的弹体状态和再入体轨迹,以实现最大射程。路径约束包括正常过载约束,动压约束和加热速率约束。控制约束包括迎角约束和倾斜角约束。初始/最终状态约束包括高度约束,速度约束和飞行路径角度约束。面对由伪谱方法得出的最优控制解的范围可能不平滑的事实,在优化中提出了虚拟控制变量(迎角和倾斜角的二阶导数),而迎角和倾斜角则为视为虚拟状态变量,以确保最佳控制解决方案的平滑性。通过仿真验证了hp自适应伪谱方法在处理非线性,多约束,多变量优化问题中的有效性,并使用该方法确定了所获得的解与间接方法最优性的一阶必要条件之间的一致性。 ate强和汉密尔顿。

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