Comprehensive compensation method for the influence of disturbing gravity field on long-range rocket guidance computing  

作　　者：Yansheng WU Zongqiang WANG Bing ZHANG 

机构地区：[1]China Aerospace Science and Technology Corporation,Beijing 100048,China [2]Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China

出　　处：《Chinese Journal of Aeronautics》2022年第3期408-418,共11页中国航空学报（英文版）

基　　金：supported by National Basic Research Program of China(No.613222)。

摘　　要：With the improvement of the accuracy of the inertial system,the influence of the disturbing gravity field on the accuracy of long-range rocket has become increasingly prominent.However,in actual engineering,there are problems of low accuracy and being time-consuming for disturbing gravity field compensation.In view of this,this paper proposes a set of online comprehensive solutions combining disturbing gravity reconstruction and stellar correction.According to the pre-launch binding parameters,the net function assignment method is used in the navigation system to calculate disturbing gravity in the boost phase online.In the guidance system,a closed-loop guidance online compensation method is proposed based on the state-space perturbation method for the disturbing gravity in the coast phase.At the same time,the vertical deflection can also be corrected by stellar guidance.The calculation results are simulated and verified under different circumstances.Simulation results show that the proposed online compensation algorithm has an accuracy improvement compared with the element compensation algorithm on ground.And the stellar guidance algorithm can further correct the impact deviation.The impact deviation after comprehensive compensation does not exceed 50 m,and the compensation percentage is greater than 65%.

关 键 词：Disturbing gravity field Long-range rocket Online compensation Stellar guidance Vertical deflection 

分 类 号：V448.1[航空宇航科学与技术—飞行器设计]