Unmanned Aerial Vehicle Guidance for an All-Aspect Approach to a Stationary Point

被引:27
作者
Ghosh, Satadal [1 ]
Yakimenko, Oleg A. [1 ]
Davis, Duane T. [2 ]
Chung, Timothy H. [3 ]
机构
[1] Naval Postgrad Sch, Dept Syst Engn, Monterey, CA 93943 USA
[2] Naval Postgrad Sch, Dept Syst Engn, Cyber Acad Grp, Monterey, CA 93943 USA
[3] Def Adv Res Projects Agcy, Tact Technol Off, Arlington, VA 22203 USA
关键词
IMPACT-ANGLE-CONTROL; CIRCULAR-NAVIGATION-GUIDANCE; SLIDING-MODE GUIDANCE; PROPORTIONAL NAVIGATION; TERMINAL GUIDANCE; CONSTRAINED GUIDANCE; MISSILE GUIDANCE; INTERCEPT-ANGLE; LAW; TIME;
D O I
10.2514/1.G002614
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper offers an integrated framework enabling planar and spatial guidance for a fixed-wing aerial vehicle to approach a stationary point from any direction. Specifically, it elaborates on the standard and two-stage pure proportional navigation guidance laws developed earlier and proposes an integrated multiphase planar guidance scheme for the all-aspect approach while also accounting for an onboard seeker's field-of-view limitation. This scheme is further extended to a two-plane-segregated two-planar-phase guidance scheme for achieving any terminal approach vector at a stationary point in three-dimensional space. The developed algorithms are evaluated in computer and software-in-the-loop simulations involving a model of a small unmanned aerial vehicle equipped with a commercial-off-the-shelf autopilot.
引用
收藏
页码:2871 / 2888
页数:18
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