TY - GEN
T1 - A guidance law design using the combination of ISMC and SDRE schemes
AU - Liang, Yew-Wen
AU - Chen, Jun Yu
AU - Lin, Li Gang
PY - 2013/11/18
Y1 - 2013/11/18
N2 - This paper studies the design of a robust guidance law for missiles in the presence of uncertainties, which may include inaccurate prediction of target maneuver. Under the design, the closed-loop guidance system is shown to be robust to the uncertainties. Additionally, the scheme presented possesses the flexibility of allowing the engineer to select a desired guidance law for the nominal system (i.e., system without uncertainty) so that the state response of the overall uncertain guidance system is close to that of the selected nominal closed-loop guidance system. The simulation results demonstrate the benefits of the presented scheme.
AB - This paper studies the design of a robust guidance law for missiles in the presence of uncertainties, which may include inaccurate prediction of target maneuver. Under the design, the closed-loop guidance system is shown to be robust to the uncertainties. Additionally, the scheme presented possesses the flexibility of allowing the engineer to select a desired guidance law for the nominal system (i.e., system without uncertainty) so that the state response of the overall uncertain guidance system is close to that of the selected nominal closed-loop guidance system. The simulation results demonstrate the benefits of the presented scheme.
UR - http://www.scopus.com/inward/record.url?scp=84887425545&partnerID=8YFLogxK
U2 - 10.1109/ICSSE.2013.6614634
DO - 10.1109/ICSSE.2013.6614634
M3 - Conference contribution
AN - SCOPUS:84887425545
SN - 9781479900091
T3 - ICSSE 2013 - IEEE International Conference on System Science and Engineering, Proceedings
SP - 63
EP - 67
BT - ICSSE 2013 - IEEE International Conference on System Science and Engineering, Proceedings
Y2 - 4 July 2013 through 6 July 2013
ER -