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作 者:Heng JING Zixuan ZHENG Dejia CHE Jianping YUAN
机构地区:[1]National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an 710072,China [2]School of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China
出 处:《Chinese Journal of Aeronautics》2024年第9期417-432,共16页中国航空学报(英文版)
基 金:supported by the National Natural Science Foundation of China (No.6200326).
摘 要:Inertial characteristics of non-cooperative targets are crucial for space capture and sub-sequent on-orbit servicing.Previous methods for identifying inertial parameters involve proximity operations,which are associated with the risk of collision with non-cooperative targets.This paper introduces a long-range,contactless method for identifying the inertial parameters of a non-cooperative target during the pre-capture phase.Specifically,electrostatic interaction is used as an external excitation to alter the target's motion.A force estimation algorithm that uses measure-ments from visual and potential sensors is proposed to estimate the electrostatic interaction and eliminate the need for force sensors.Furthermore,a recursive estimation-identification framework is presented to concurrently estimate the coupled motion state,weak electrostatic interaction,and inertial parameters of the target.The simulation results show that the proposed method extends the identification distance to 170 times that of the previous method while maintaining high identifica-tion precision forall parameters.
关 键 词:Non-cooperative target Inertial parameters identification Electrostatic interaction Force estimation Dynamical coupling
分 类 号:V448[航空宇航科学与技术—飞行器设计]
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