Mathematics
Logic
Scientist
Shanghai Institute of Satellite Engineering, Shanghai 200240, China
College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Command generator tracker based direct model reference adaptive tracking guidance for Mars atmospheric entry
Mars entry trajectory optimization using DOC and DCNLP
MCAV/IMU integrated navigation for the powered descent phase of Mars EDL
Radio beacons/IMU integrated navigation for Mars entry
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