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首页> 外文期刊>Transactions of the Japan society for aeronautical and space sciences >Low-Thrust, Multi-Revolution Orbit Transfer under the Constraint of a Switch Function without Prior Information
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Low-Thrust, Multi-Revolution Orbit Transfer under the Constraint of a Switch Function without Prior Information

机译:无先验信息的切换功能约束下的低推力多旋转轨道转移

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摘要

In this paper, a low-thrust, multi-revolution orbit transfer under the constraint of a complex switch function is investigated. First, the effect of the switch function, especially that of a switch function with no prior information, is analyzed. Then, by utilizing the concept of the Lyapunov feedback control law, the semi-analytical expressions of subop-timal thrust angles are derived, and a near-optimal solution could approach the optimal solution by adjusting the five weights in the Lyapunov function using sequential quadratic programming (SQP). In the novel method, except for optimization of the weight factors in the Lyapunov function, no iteration is contained in the process of design and optimization, so the method is rapid and has good convergence. This method also overcomes the drawbacks about convergence of traditional calculus of variation (COV). It is an effective method for the design of low-thrust, multi-revolution orbit transfer with no prior information switch functions.
机译:本文研究了在复杂开关函数约束下的低推力多旋转轨道传递。首先,分析开关功能的效果,尤其是没有先验信息的开关功能的效果。然后,利用李雅普诺夫反馈控制律的概念,推导了次最优推力角的半解析表达式,并通过使用连续二次函数调整李雅普诺夫函数中的五个权重,使近似最优解可以逼近最优解。编程(SQP)。在该新方法中,除了优化Lyapunov函数中的权重因子外,在设计和优化过程中不包含迭代,因此该方法快速且具有良好的收敛性。该方法还克服了传统变分演算(COV)收敛的缺点。这是设计低推力,多次旋转轨道转移的有效方法,无需先验信息转换功能。

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