A Ballistic Reconstruction Algorithm for Attitude-Orbit Coupling Low-Thrust Maneuver
Author:
Affiliation:
1. State Key Laboratory of Astronautic Dynamics,Xi'an,China,710043
2. Xi'an Huanyu Satellite Control and Data Application Co. Ltd,Xi'an,China,710043
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10239690/10239711/10241010.pdf?arnumber=10241010
Reference16 articles.
1. Adaptive sampling for near space hypersonic gliding target tracking;ding;Journal of Beijing Institute of Technology,2022
2. Adaptive extended kalman filter for ballistic missile tracking;kumar;International Journal of Electrical and Computer Engineering,2017
3. A jerk model for tracking highly maneuvering targets
4. An adaptive attitude algorithm based on a current statistical model for maneuvering acceleration
5. Orbit determination and thrust force modeling for a maneuvered GEO satellite using two-way adaptive Kalman filtering
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