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软着陆小行星的自主导航与制导
引用本文:崔祜涛,崔平远.软着陆小行星的自主导航与制导[J].宇航学报,2002,23(5):1-4,10.
作者姓名:崔祜涛  崔平远
作者单位:哈尔滨工业大学深空探测基础研究中心,哈尔滨,150001
基金项目:国防科工委民用航天科研计划资助
摘    要:讨论了软着陆小行星的自主导航与制导问题,首先给出了一种使用星上光学相机和激光雷达的自主导航方法,测量探测器相对着陆点的距离与速度;接着提出了一种自主软着陆的制导方案,为了保证垂直软着陆,事先规划了满足约束的理想下降高度与速度轨迹,并设计滑模变结构控制器跟踪理想轨迹,实现在小行星表面垂直软着陆。最后通过数学仿真验证了提出的自主光学导航与制导方法的可行性。

关 键 词:软着陆  行星  自主导航  制导
文章编号:1000-1328(2002)05-0001-04

Autonomous navigation and guidance for soft-landing asteroid
CUI Hu tao,CUI Ping yuan.Autonomous navigation and guidance for soft-landing asteroid[J].Journal of Astronautics,2002,23(5):1-4,10.
Authors:CUI Hu tao  CUI Ping yuan
Abstract:In this paper,we discussed the problem of autonomous optical guidance and navigation for descent to a small body.First,an autonomous optical navigation method using on board optical camera and laser radar was given to measure relative position and velocity between probe and asteroid,and then an autonomous guidance strategy was proposed.A prescribed altitude and velocity profile was defined to ensure vertical soft landing.A sliding mode controller was designed to track prescribed altitude and velocity profile for safely soft landing on surface of small body.Finally,simulations are conducted to verify the guidance precision.The effects for the guidance precision of varies perturbation including observation errors,initial state errors,parameter errors is discussed.
Keywords:Soft  landing for small asteroid  Autonomous navigation  Autonomous control
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