在SE上用几何精确计算的刚体最优控制（3）
Optimal Control of a Rigid Body using Geometrically Exact Computations on SE(3)
摘要：
本文提出了三维刚体轨道和转动联合机动的最优控制问题和有效的计算方法。假定刚体在力和力矩的影响下起作用，这些力和力矩是由势和控制力和力矩产生的。本文的主要特点是它使用的计算程序，保证保持几何的最优解。理论基础的计算程序进行了总结，最佳航天器机动的例子。
英文摘要：
Optimal control problems are formulated and efficient computational procedures are proposed for combined orbital and rotational maneuvers of a rigid body in three dimensions. The rigid body is assumed to act under the influence of forces and moments that arise from a potential and from control forces and moments. The key features of this paper are its use of computational procedures that are guaranteed to preserve the geometry of the optimal solutions. The theoretical basis for the computational procedures is summarized, and examples of optimal spacecraft maneuvers are presented.
机构、总结、中文摘要均由AI分析而来，可能存在错误，请以论文正文为准。
