Author/Authors :
Bahrami, M amirkabir university of technology - Department Mechanical Engineering, تهران, ايران , Ebrahimi, B Aerospace Research Institute, Ministry of Science, Research, and Technology, ايران , Roshanian, J k.n.toosi university of technology - Department Aerospace, تهران, ايران
Abstract :
An optimal strategy based on minimum effort control and also with terminal position constraint is developed for an exoatmospheric interceptor with a fixed- interval guidance time. It is then integrated with sliding-mode control theory to drive an optimal sliding-mode guidance law for fixed-interval guidance time. In addition, this guidance law is generalized for intercepting an arbitrarily time-varying target maneuver. Robustness of the new guidance method against disturbances and good miss distance performance are achieved by the second method of Lyapunov and simulation results. The presented guidance law is simple to implement in practical applications.
