In this paper a novel terminal guidance law for hypersonic vehicle is investigated. In order to accelerate the convergence rate of line of sight angle, adding a power integrator technique based nonlinear guidance law which can make the line of sight converge to zero in finite time is proposed. Then rigorous stability analysis of finite-time convergence is shown. It demonstrates the effectiveness of the approach by numerical simulation meanwhile the approach have strong robustness in the presence of disturbance.
Adding a power integrator technique based terminal guidance law
01.08.2016
206231 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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