Three-Dimensional Formation Guidance with Rigidly Connected Virtual Leaders

被引:2
作者
Tekin, Raziye [1 ]
Erer, Koray S. [1 ]
机构
[1] Roketsan Missiles Inc, Tact Missile Syst, TR-06780 Ankara, Turkey
关键词
LAWS;
D O I
10.2514/1.G005850
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:1229 / 1236
页数:8
相关论文
共 19 条
[1]   Flying in formation using a pursuit guidance algorithm [J].
Betser, A ;
Vela, PA ;
Pryor, G ;
Tannenbaum, A .
ACC: PROCEEDINGS OF THE 2005 AMERICAN CONTROL CONFERENCE, VOLS 1-7, 2005, :5085-5090
[2]   NLDI guidance control laws for close formation flight [J].
Campa, G ;
Seanor, B ;
Gu, Y ;
Napolitano, MR .
ACC: Proceedings of the 2005 American Control Conference, Vols 1-7, 2005, :2972-2977
[3]  
Challa V., 2018, AIAA SCITECH FOR
[4]  
Erer KS, 2016, MED C CONTR AUTOMAT, P238, DOI 10.1109/MED.2016.7535912
[5]  
Jacques D., 2001, GUID NAV CONTR COL C, DOI 10.2514/6.2001-4075
[6]  
Jenkinson L.R., 1995, AIAA AIRCR ENG TECHN
[7]  
Kilic M.C., 2020, THESIS CLAUSTHAL U T
[8]  
Lee J.E., 2008, KSAS INT J, V9, P71, DOI [10.5139/IJASS.2008.9.2.071, DOI 10.5139/IJASS.2008.9.2.071]
[9]   Synthetic-Waypoint Guidance Algorithm for Following a Desired Flight Trajectory [J].
Medagoda, Eran D. B. ;
Gibbens, Peter W. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (02) :601-606
[10]  
Osteroos R.K., 2002, AFFTCTIM0408