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Published in 2020 at "Chinese Journal of Aeronautics"
DOI: 10.1016/j.cja.2019.07.013
Abstract: Abstract Guidance laws are proposed for a near space interceptor with on–off type thrust as output. The target-interceptor engagement kinematics is integrated with the first-order dynamics of thruster to design guidance laws. The bang-bang type…
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Keywords:
finite time;
composite guidance;
guidance;
guidance law ... See more keywords