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Research on trajectory optimization of powered flight for strong coupling and multi-constraints vehicle

机译:强耦合多约束飞行器动力飞行轨迹优化研究

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摘要

An integrated trajectory optimization method for strong coupling and multi-constraints vehicle is presented. Based on thecharacteristics of strong coupling and multi-constraints, considering the change rate of angle of attack and safety marginof scramjet as additional constraint conditions and taking the minimum coupling degree as optimization index, thereference trajectory is adopted, which uses a smoothing method for solving multi-constraint s optimal problems. Thereference trajectory can avoid the scramjet being in unsafe working condition to a certain extent, and also can greatlyimprove the accuracy of reference trajectory tracking. Based on the precise simulation model, the simulation analysis iscarried out. The simulation results show that the method is effective and reliable.
机译:提出了一种用于强耦合多约束车辆的综合轨迹优化方法。基于 考虑攻角变化率和安全裕度的强耦合和多约束特性 以超燃冲压发动机作为附加约束条件,并以最小耦合度作为优化指标, 采用了参考轨迹,它使用平滑方法来解决多约束的最优问题。这 参考轨迹可以在一定程度上避免超燃冲压发动机处于不安全的工作状态,并且可以大大 提高参考轨迹跟踪的准确性。基于精确的仿真模型,仿真分析为 执行。仿真结果表明该方法是有效和可靠的。

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