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作 者:Kebo LI Zhihui BAI Hyo-Sang SHIN Antonios TSOURDOS Min-Jea TAHK
机构地区:[1]Department of Applied Mechanics,College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China [2]Institute of Aerospace Sciences,SATM,Cranfield University,Cranfield MK430AL,UK [3]Department of Aerospace Engineering,Korea Advanced Institute of Science and Technology,Daejeon 34141,Republic of Korea
出 处:《Chinese Journal of Aeronautics》2022年第7期75-90,共16页中国航空学报(英文版)
基 金:supported in part by the National Natural Science Foundation of China(No.12002370);in part by the Hunan Provincial Natural Science Foundation of China(No.2019JJ50736)。
摘 要:The capturability of the Three-Dimensional(3D)Realistic True Proportional Navigation(RTPN)guidance law is thoroughly analyzed.The true-arbitrarily maneuvering target is considered,which maneuvers along an arbitrary direction in 3D space with an arbitrary but upperbounded acceleration.The whole nonlinear relative kinematics between the interceptor and target is taken into account.First,the upper-bound of commanded acceleration of 3D RTPN is deduced,using a novel Lyapunov-like approach.Second,the reasonable selection range of navigation gain of3D RTPN is analyzed,when the maneuver limitation of interceptor is considered.After that,a more realistic definition of capture is adopted,i.e.,the relative range is smaller than an acceptable miss-distance while the approaching speed is larger than a required impact speed.Unlike previous researches which present Two-Dimensional(2D)capture regions,the inequality analysis technique is utilized to obtain the 3D capture region,where the three coordinates are the closing speed,transversal relative speed,and relative range.The obtained capture region could be taken as a sufficient-but-unnecessary condition of capture.The new theoretical findings are all given in explicit expressions and are more general than previous results.
关 键 词:Capture region Lyapunov-like approach Maneuverability Limitation Realistic true proportional navigation True-arbitrarily maneuvering target
分 类 号:V249.3[航空宇航科学与技术—飞行器设计] V448
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