首页> 外文会议>International astronautical congress >A NOVEL NONLINEAR GUIDANCE SCHEME FOR POWER-LIMITED AUTONOMOUS RENDEZVOUS WITH FIXED DOCKING DIRECTION AND COLLISION AVOIDANCE CONSTRANITS
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A NOVEL NONLINEAR GUIDANCE SCHEME FOR POWER-LIMITED AUTONOMOUS RENDEZVOUS WITH FIXED DOCKING DIRECTION AND COLLISION AVOIDANCE CONSTRANITS

机译:具有固定对接方向和碰撞规避性的功率受限自动交会的新型非线性指导方案

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This paper solves the problem of optimal guidance scheme of a powered chaser and a passive target in a highly elliptical orbit. The Tschauner-Hempel equations are derived to describe the relative motion. Then, the rendezvous problems are explicitly formulated as an online trajectory planning problem by using the proposed method. Furthermore, the limitation of thruster activation is considered. Meanwhile, in order to fully demonstrate the performance of the guidance algorithm, the effects of eccentricity and prediction horizon on the time consumption and control expenditure is studied. Finally, simulations are implemented with different scenarios by using Matlab, and the results illustrate this method can deal with both circular and elliptical case, which can be used to generate the fuel-optimal trajectory on-line rapidly.
机译:本文解决了高椭圆轨道上动力追赶者和被动目标的最优制导方案问题。推导了Tschauner-Hempel方程来描述相对运动。然后,使用所提出的方法将交会问题明确地表述为在线轨迹规划问题。此外,考虑了推进器启动的限制。同时,为了充分证明制导算法的性能,研究了离心率和预测范围对时间消耗和控制支出的影响。最后,使用Matlab在不同的场景下进行了仿真,结果表明该方法可以处理圆形和椭圆形情况,可用于快速在线生成最佳燃油轨迹。

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