Rapid Trajectory Optimization of Continuous-Low-Thrust Spacecraft Based on Bezier Shape Function and Inverse Dynamics
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-8045-1_22
Reference23 articles.
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3. Wall BJ, Conway BA (2009) Shape-based approach to low-thrust rendezvous trajectory design. J Guid Control Dyn 32(1):95–101
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5. Xie C, Zhang G, Zhang YC (2015) Simple shaping approximation for low-thrust trajectories between coplanar elliptical orbits. J Guid Control Dyn 38(12):2448–2455
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