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Investigation of the Stability of Satellite Large Angle Attitude Manoeuvres Using Nonlinear Optimization Methods

机译:卫星大角度姿态机动稳定性的非线性优化研究。

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摘要

Some theoretical investigations of large angle attitude manoeuvres have been based on the application of Lyapunov's stability theory. With this method Mortensen derived stable control laws for performing attitude manoeuvres with either thrusters or reaction wheels. Previous results were idealized in that they ignored the nonlinearities inherent in the operation of both types of actuators. The present paper extends the scope of this work by acknowledging the actuator nonlinearities. The approach selected is to estimate the domain of attraction (DOA) of the target equilibrium for the system corresponding to the idealized control laws constrained by the actuator nonlinearities. The DOA is estimated by searching for the largest region of asymptotic stability over a set of quadratic Lyapunov functions. This approach results from the application of a theorem of Lasalle and gives rise to two nested nonlinear optimization problems, the internal one of which is a constrained global problem with several local minima. The paper gives an overview of the progress made in solving problems of this complexity. Emphasis has been placed on the parametrization of quadratic Lyapunov functions and a detailed comparison of several candidate nonlinear optimization techniques has been made for both the constrained and unconstrained optimization problem. Areas requiring further research are identified.
机译:基于李雅普诺夫稳定性理论的应用,对大角度姿态机动进行了一些理论研究。通过这种方法,Mortensen得出了稳定的控制定律,可通过推进器或反作用轮进行姿态操纵。先前的结果是理想的,因为它们忽略了两种类型的执行器操作中固有的非线性。通过承认执行器的非线性,本文扩展了这项工作的范围。选择的方法是针对与执行器非线性约束的理想控制定律估计系统的目标平衡的吸引域(DOA)。通过在一组二次Lyapunov函数上搜索最大渐近稳定性区域来估算DOA。这种方法是由Lasalle定理的应用产生的,并产生了两个嵌套的非线性优化问题,其中一个是内部的,是一个具有多个局部极小值的约束全局问题。本文概述了解决这种复杂性问题所取得的进展。重点放在二次Lyapunov函数的参数化上,并针对约束和非约束优化问题对几种候选非线性优化技术进行了详细比较。确定需要进一步研究的领域。

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