A Semi-Analytic Approach for Trajectory Design Optimization Using Linearized Equations of Motion-Reference-Cited by-同舟云学术

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A Semi-Analytic Approach for Trajectory Design Optimization Using Linearized Equations of Motion

Published:2023-06-07 Issue: Volume: Page:
ISSN:
Container-title:2023 10th International Conference on Recent Advances in Air and Space Technologies (RAST)
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Author:

Negrete Aimar¹,Vijayakumar Madusudan¹,Abdelkhalik Ossama¹

Affiliation:

1. Iowa State University,Department of Aerospace Engineering,Ames,USA

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10197839/10197652/10197970.pdf?arnumber=10197970

Reference17 articles.

1. Take-Off from Satellite Orbit

2. Constant Radial Thrust Acceleration Redux

3. Escape From a Circular Orbit Using Tangential Thrust

4. Escape from Elliptic Orbit Using Constant Radial Thrust

5. Shape-Based Approach for Low-Thrust Earth–Moon Trajectories Initial Design

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