TY - GEN
T1 - A nonlinear adaptive guidance law for missile interceptions
AU - Liang, Hongwei
AU - Ma, Baoli
PY - 2008
Y1 - 2008
N2 - A nonlinear adaptive guidance law is derived for the model of planar missile interception. The proposed guidance law guarantees that the missile can intercept a maneuverable target with unknown constant (piece-wise constant) angular velocity. Compared with the previous results, the proposed one efficiently use the measurable information, and does not need to use variable structure control terms to circumvent the motion uncertainty of the target, and thus is smooth and can be easily implemented. Simulation results verify the effectiveness of the proposed guidance law.
AB - A nonlinear adaptive guidance law is derived for the model of planar missile interception. The proposed guidance law guarantees that the missile can intercept a maneuverable target with unknown constant (piece-wise constant) angular velocity. Compared with the previous results, the proposed one efficiently use the measurable information, and does not need to use variable structure control terms to circumvent the motion uncertainty of the target, and thus is smooth and can be easily implemented. Simulation results verify the effectiveness of the proposed guidance law.
KW - Adaptive control
KW - Missile interception
KW - Nonlinear guidance law
UR - https://www.scopus.com/pages/publications/52449107069
U2 - 10.1109/CHICC.2008.4605316
DO - 10.1109/CHICC.2008.4605316
M3 - 会议稿件
AN - SCOPUS:52449107069
SN - 9787900719706
T3 - Proceedings of the 27th Chinese Control Conference, CCC
SP - 342
EP - 344
BT - Proceedings of the 27th Chinese Control Conference, CCC
T2 - 27th Chinese Control Conference, CCC
Y2 - 16 July 2008 through 18 July 2008
ER -