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进入角约束下的载机变结构远距引导
引用本文:俞吉,周德云,马云红,周灿辉.进入角约束下的载机变结构远距引导[J].指挥控制与仿真,2013,35(4):108-111,117.
作者姓名:俞吉  周德云  马云红  周灿辉
作者单位:西北工业大学,西北工业大学,西北工业大学,中国电子科技集团第二十八研究所
摘    要:针对一般导引律在载机远距引导中存在的问题,结合远距引导的需求,设计了远距引导的三维变结构导引律。该导引律具有较强自适应性,可以使载机以期望的进入角接近目标。仿真结果表明,载机在该导引律作用下,能以较小过载,平滑轨迹快速接近机动目标,并保证载机引导结束时占有有利的空中战术态势。

关 键 词:远距引导  进入角约束  变结构  制导律
修稿时间:4/7/2013 12:00:00 AM

Study on a Long-Distance Navigation Method with Entrance Angle Constraints for Vehicles Based on Variable Structure
Yu Ji,zhou de yun,ma yun hong and zhou can hui.Study on a Long-Distance Navigation Method with Entrance Angle Constraints for Vehicles Based on Variable Structure[J].Command Control & Simulation,2013,35(4):108-111,117.
Authors:Yu Ji  zhou de yun  ma yun hong and zhou can hui
Institution:Northwestern Polytechnical University,Norhwestern Polytechnical University,Norhwestern Polytechnical University,China Electronics Technology Group Corporation 28th Research Institute
Abstract:A three-dimensional guidance low based on variable structure was designed according to the requirement of long-distance navigation, which can lead the attackers to the target with the desired entrance angle self-adaptively. Simulation results show the attackers can approach the targets quickly even if the targets maneuver acutely with the minor normal acceleration and smoothing trajectory, and can keep its tactical advantages at the ending of navigation.
Keywords:long-distance navigation    entrance angle constraint    variable structure    guidance low
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