Prescribed performance interceptor guidance with terminal line of sight angle constraint accounting for missile autopilot lag
Author:
Funder
China Scholarship Council
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference23 articles.
1. A guidance law with terminal impact angle constraint accounting for missile autopilot;Zhou;J. Dyn. Syst. Meas. Control,2013
2. Robust terminal angle constraint guidance law with autopilot lag for intercepting maneuvering targets;He;Nonlinear Dyn.,2015
3. Guidance laws with finite time convergence;Zhou;J. Guid. Control Dyn.,2009
4. Intercept-angle guidance;Shima;J. Guid. Control Dyn.,2011
5. Finite-time convergent guidance law with impact angle constraint based on sliding mode control;Zhang;Nonlinear Dyn.,2012
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