TY - GEN
T1 - A novel mid-course doctrine for multiple flight vehicles cooperative interception
AU - Wang, Long
AU - Yao, Yu
AU - He, Fenghua
AU - Liu, Kai
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2017/1/20
Y1 - 2017/1/20
N2 - In this paper, we consider the problem of intercepting a target with large information uncertainties during the mid-course guidance, which will result in a large inertial error of the terminal guidance. In order to improve the interception probability, multiple intercepting flight vehicles are employed. Taking the information transmission between the flight vehicles into consideration, a novel cooperative doctrine for mid-course guidance is proposed to guarantee the interception probability with fewer intercepting flight vehicles. Then in order to maximize the interception probability of the target, an optimization problem is established to design the optimal relative motion parameters between the flight vehicle and target at the handover moment, as well as the optimal interval between the handover time of different flight vehicles. A preliminary approach is proposed and simulation experiments are carried out to show the feasibility of the proposed cooperative doctrine.
AB - In this paper, we consider the problem of intercepting a target with large information uncertainties during the mid-course guidance, which will result in a large inertial error of the terminal guidance. In order to improve the interception probability, multiple intercepting flight vehicles are employed. Taking the information transmission between the flight vehicles into consideration, a novel cooperative doctrine for mid-course guidance is proposed to guarantee the interception probability with fewer intercepting flight vehicles. Then in order to maximize the interception probability of the target, an optimization problem is established to design the optimal relative motion parameters between the flight vehicle and target at the handover moment, as well as the optimal interval between the handover time of different flight vehicles. A preliminary approach is proposed and simulation experiments are carried out to show the feasibility of the proposed cooperative doctrine.
UR - https://www.scopus.com/pages/publications/85015166774
U2 - 10.1109/CGNCC.2016.7828793
DO - 10.1109/CGNCC.2016.7828793
M3 - 会议稿件
AN - SCOPUS:85015166774
T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
SP - 252
EP - 257
BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Y2 - 12 August 2016 through 14 August 2016
ER -