TY - GEN
T1 - Estimation enhancement by imposing a relative intercept angle for defending missiles
AU - Fonod, Robert
AU - Shima, Tal
N1 - Publisher Copyright: © 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - A multiple-body interception scenario is considered, where an evading target aircraft launches two defending missiles as a countermeasure against an incoming homing missile. The defenders share their respective line of sight angle measurements, are aware of the target’s evasion strategy, and exploit a cooperate guidance law which can impose a relative intercept angle between them. The ability of the proposed cooperative guidance-estimation scheme to protect the targeted aircraft is analyzed. Especially, the effect of different values of the commanded relative intercept angle on the intertwined guidance-estimation performance is studied.
AB - A multiple-body interception scenario is considered, where an evading target aircraft launches two defending missiles as a countermeasure against an incoming homing missile. The defenders share their respective line of sight angle measurements, are aware of the target’s evasion strategy, and exploit a cooperate guidance law which can impose a relative intercept angle between them. The ability of the proposed cooperative guidance-estimation scheme to protect the targeted aircraft is analyzed. Especially, the effect of different values of the commanded relative intercept angle on the intertwined guidance-estimation performance is studied.
UR - http://www.scopus.com/inward/record.url?scp=85088071532&partnerID=8YFLogxK
U2 - https://doi.org/10.2514/6.2017-1018
DO - https://doi.org/10.2514/6.2017-1018
M3 - منشور من مؤتمر
SN - 9781624104503
T3 - AIAA Guidance, Navigation, and Control Conference, 2017
BT - AIAA Guidance, Navigation, and Control Conference, 2017
T2 - AIAA Guidance, Navigation, and Control Conference, 2017
Y2 - 9 January 2017 through 13 January 2017
ER -