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当交会时间较长时需要在轨道规划中考虑摄动的影响,本文基于虚拟瞄准点的思想,研究了考虑轨道摄动情况下的固定时间拦截问题求解方法,并提出了考虑轨道摄动影响的多冲量交会规划方法。通过仿真算例验证了算法的有效性,并对基于二体模型和考虑摄动的规划结果进行了对比。
Considering the influence of perturbation in orbit planning when the rendezvous time is longer, based on the idea of virtual aiming point, a method of solving fixed time interception problem considering orbital perturbation is studied. Multi-impact intersection planning method. The simulation results show the effectiveness of the algorithm and the comparison between the two-body model and the planning results considering the perturbation.