Blinding Guidance Against Missiles Sharing Bearings-Only Measurements

被引:17
作者
Fonod, Robert [1 ]
Shima, Tal [1 ]
机构
[1] Technion Israel Inst Technol, Dept Aerosp Engn, IL-3200003 Haifa, Israel
关键词
HOMING MISSILES; ESTIMATION ENHANCEMENT; TRAJECTORY MODULATION; EVASION; OBSERVABILITY; AIRCRAFT;
D O I
10.1109/TAES.2017.2747098
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A novel "blind and evade" guidance concept for an aerial target, which is exposed to a threat of two homing missiles, is presented. Each missile is assumed to measure solely its own line-of-sight (LOS) angle and share it with the other missile. Such information sharing enables the missiles to form a triangular measuring baseline relative to the target and to improve their estimation accuracy. However, if the separation angle between the two LOS vectors is small enough, the observability of such double-LOS measuring approach becomes weak. Motivated by this observation, the idea of the proposed concept is to bring the missiles on the same LOS with the target, i.e., blinding them, and then perform an appropriately timed target evasive maneuver. The target's guidance law is derived under the assumption of perfect information and formulated as an optimal control problem. Simulation results demonstrate the potential of the proposed defense concept.
引用
收藏
页码:205 / 216
页数:12
相关论文
共 28 条
[11]  
Jackson B.A., 2008, Evaluating novel threats to the homeland: unmanned aerial vehicles and cruise missiles, V626
[12]  
Jameson A, 1981, P AIAA 14 FLUID PLAS
[13]   Time-to-go Polynomial Guidance with Trajectory Modulation for Observability Enhancement [J].
Kim, Tae-Hun ;
Lee, Chang-Hun ;
Tahk, Min-Jea .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2013, 49 (01) :55-73
[14]   ON CONCEPTS OF CONTROLLABILITY + OBSERVABILITY OF LINEAR SYSTEMS [J].
KREINDLER, E ;
SARACHIK, PE .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1964, AC 9 (02) :129-&
[15]  
Liu Y., 2013, P AIAA GUID NAV CONT
[16]   Line-of-Sight Interceptor Guidance for Defending an Aircraft [J].
Ratnoo, Ashwini ;
Shima, Tal .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2011, 34 (02) :522-532
[17]   Time-to-go weighted optimal guidance with impact angle constraints [J].
Ryoo, Chang-Kyung ;
Cho, Hangju ;
Tahk, Min-Jea .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2006, 14 (03) :483-492
[18]   Observability Analysis and Enhancement of Radome Aberration Estimation With Line-of-Sight Angle-Only Measurement [J].
Seo, Min-Guk ;
Tahk, Min-Jea .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2015, 51 (04) :3321-3331
[19]  
Shaferman V., 2009, P AIAA GUID NAV CONT, P10
[20]   Stochastic Cooperative Interception Using Information Sharing Based on Engagement Staggering [J].
Shaferman, Vitaly ;
Oshman, Yaakov .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (09) :2127-2141