弹道
可靠性(半导体)
控制(管理)
避碰
过程(计算)
计算机科学
轨迹优化
控制理论(社会学)
钥匙(锁)
工程类
碰撞
人工智能
计算机安全
量子力学
操作系统
物理
功率(物理)
天文
作者
Pingyuan Cui,Yanjie Liu,Zhengshi Yu,Shengying Zhu,Wei Shao
标识
DOI:10.1016/j.actaastro.2017.04.033
摘要
Landing exploration is an important way to improve the understanding of small bodies. Considering the weak gravity field as well as the strict attitude constraints which make bounce a common situation and a tough issue for safe landing on small bodies, a novel active trajectory control-based intelligent landing strategy is proposed to improve the safety and reliability of mission. The scenarios of intelligent landing strategy for both safe landing and hopping exploration are introduced in detail and a potential structure for autonomous navigation and control system is presented. Furthermore, a convex optimization-based control algorithm is developed, which is the key technology fulfilling the active trajectory control. Meanwhile a novel discretization method based on the fourth-order Runge-Kutta rule is proposed to improve the accuracy. A helpful adjustment process of time-to-landing is also introduced when the feasible trajectory does not exist. Comprehensive simulations about the proposed intelligent landing strategy are performed to demonstrate the improved safety and accuracy of both landing and hopping exploration on small bodies. Meanwhile, the performance and accuracy of the proposed convex optimization-based control algorithms is also compared and discussed thoroughly. Some useful conclusions for control system design are also obtained.
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