Up to now the singular optimal control problems in the thrust synergetic orbital transfer have not been completely solved.
特别是由推力协同变轨所导致的奇异最优控制问题到目前尚没有完全解决。
In this paper, an analytical design method for time-optimal servomechanisms with high accuracy based on singular optimal control principles is described.
本文介绍了把奇异最优控制原理用于高精度快速随动系统的分析设计方法。
The study results show that some constrained optimal control problems can be solved efficiently with the improved algorithm, including some singular optimal control problems.
结果表明，改进算法能较好地求解一类受约束最优控制问题，对奇异最优控制问题也能较好求解。
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