TY - GEN
T1 - Adaptive sliding-mode guidance with terminal angle constraints based on explicit space engagement model
AU - Yun, Yuhang
AU - Tang, Shengjing
AU - Guo, Jie
AU - Zhou, Yunqiang
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2017/1/20
Y1 - 2017/1/20
N2 - In this paper, an explicit guidance model of space movement for air to ground missile has been built by deducing the transitions of parameters between two dimensional plane and space movement, such as velocities, angles and angular rates. Afterwards an adaptive sliding-mode guidance law is deduced on the basis of the proposed model, which satisfies the intercept angular constraints in both longitudinal plane and lateral plane. Simulations are carried out and demonstrate the effectiveness of the stated method.
AB - In this paper, an explicit guidance model of space movement for air to ground missile has been built by deducing the transitions of parameters between two dimensional plane and space movement, such as velocities, angles and angular rates. Afterwards an adaptive sliding-mode guidance law is deduced on the basis of the proposed model, which satisfies the intercept angular constraints in both longitudinal plane and lateral plane. Simulations are carried out and demonstrate the effectiveness of the stated method.
KW - Explicit guidance model
KW - Sliding-mode guidance
KW - Terminal angle constraints
UR - http://www.scopus.com/inward/record.url?scp=85015152783&partnerID=8YFLogxK
U2 - 10.1109/CGNCC.2016.7828949
DO - 10.1109/CGNCC.2016.7828949
M3 - Conference contribution
AN - SCOPUS:85015152783
T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
SP - 1144
EP - 1147
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 -