TY - GEN
T1 - Optimal linear-quadratic guidance law considering autopilot first-order lag with terminal acceleration constraint
AU - Zheng, Duo
AU - Xu, Xinghua
AU - Yan, Ruyi
AU - Lin, Defu
N1 - Publisher Copyright:
© Springer Nature Singapore Pte Ltd. 2019.
PY - 2019
Y1 - 2019
N2 - In this paper, a new optimal linear-quadratic guidance law with terminal acceleration constraints is proposed for intercepting maneuvering target. Because the angle of attack is approximately proportional to the normal acceleration for aerodynamic control missile, not only miss distance, but also terminal acceleration is required to converge to zero for increasing effectiveness of the warhead for destroying armored target in the proposed guidance law. The gain characteristic of proposed guidance law is studied by comparing with traditional optimal guidance law with considering autopilot dynamics lags. Numerical simulations are performed to examine performance of the proposed optimal guidance law, and its robustness with respect to the time constant of autopilot dynamic lags is also studied by considering time constant typical errors.
AB - In this paper, a new optimal linear-quadratic guidance law with terminal acceleration constraints is proposed for intercepting maneuvering target. Because the angle of attack is approximately proportional to the normal acceleration for aerodynamic control missile, not only miss distance, but also terminal acceleration is required to converge to zero for increasing effectiveness of the warhead for destroying armored target in the proposed guidance law. The gain characteristic of proposed guidance law is studied by comparing with traditional optimal guidance law with considering autopilot dynamics lags. Numerical simulations are performed to examine performance of the proposed optimal guidance law, and its robustness with respect to the time constant of autopilot dynamic lags is also studied by considering time constant typical errors.
KW - Autopilot dynamics lags
KW - Optimal guidance law
KW - Robustness with time constant
KW - Terminal acceleration constraint
KW - Terminal zero angle of attack
UR - http://www.scopus.com/inward/record.url?scp=85070785744&partnerID=8YFLogxK
U2 - 10.1007/978-981-13-3305-7_187
DO - 10.1007/978-981-13-3305-7_187
M3 - Conference contribution
AN - SCOPUS:85070785744
SN - 9789811333040
T3 - Lecture Notes in Electrical Engineering
SP - 2310
EP - 2330
BT - The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018
A2 - Zhang, Xinguo
PB - Springer Verlag
T2 - Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018
Y2 - 16 October 2018 through 18 October 2018
ER -