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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.
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页码:2871 / 2888
页数:18
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