Entry guidance with terminal approach angle constraint
Author:
Funder
National Natural Science Foundation of China
National Key R&D Program of China
Beijing Institute of Technology Research Fund Program for Young Scholars
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference28 articles.
1. Verification of a fully numerical entry guidance algorithm;Lu;J. Guid. Control Dyn.,2017
2. Multiple method 2-D trajectory optimization satisfying waypoints and no-fly zone constraints;Jorris;J. Guid. Control Dyn.,2008
3. Reentry trajectory optimization with waypoint and no-fly zone constraints using multiphase convex programming;Zhao;Acta Astronaut.,2017
4. Rapid generation of entry trajectories with waypoint and no-fly zone constraints;Xie;Acta Astronaut.,2012
5. Three-dimensional trajectory optimization satisfying waypoint and no-fly zone constraints;Jorris;J. Guid. Control Dyn.,2009
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