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
相关论文
共 50 条
[1]  
[Anonymous], 2016, JSBSIM OP SOURC FLIG
[2]  
[Anonymous], 2016, SITL SIM SOFTW LOOP
[3]  
Apostol T. M, 2002, MATH ANAL, p[127, 140]
[4]   Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law [J].
Bardhan, Rajarshi ;
Ghose, Debasish .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (03) :384-402
[5]  
Chabra S, 2007, DEFENCE SCI J, V57, P497
[6]   Optimal Impact Angle Control Guidance Law Based on Linearization About Collision Triangle [J].
Cho, Hangju ;
Ryoo, Chang-Kyung ;
Tsourdos, Antonios ;
White, Brian .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2014, 37 (03) :958-964
[7]  
Chung TH, 2016, IEEE INT CONF ROBOT, P1255, DOI 10.1109/ICRA.2016.7487257
[8]  
Clark M, 2016, AIAA GUID NAV CONTR, DOI [10.2514/6.2016-1986, DOI 10.2514/6.2016-1986]
[9]  
Clark M., 2017, AIAA INFORM SYSTEMS, DOI [10.2514/6.2017-0672, DOI 10.2514/6.2017-0672]
[10]  
Day MA, 2015, INT CONF UNMAN AIRCR, P426, DOI 10.1109/ICUAS.2015.7152319