Abstract
This study addresses a systematic application of the attitude-dependent solar radiation pressure (SRP) to designing frozen orbits near small bodies subject to the dynamic environment of up to the fourth zonal effects for a long-term analysis on orbit-attitude coupled motions. It begins with selecting SRP models tailored to orbit-attitude coupled dynamics. A desired SRP model for that purpose should be capable of addressing both force and torque. Additionally, this study outlines a strategy for integrating the selected SRP model into the frozen orbit design. It first averages the SRP over both orbit and attitude, and re-aligns the first axis on the average SRP. Numerical simulations indicate that the proposed strategy is effective in maintaining average variations in orbital elements to be small.
Original language | English |
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Title of host publication | AIAA SciTech Forum and Exposition, 2024 |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624107115 |
DOIs | |
Publication status | Published - 2024 |
Event | AIAA SciTech Forum and Exposition, 2024 - Orlando, United States Duration: 2024 Jan 8 → 2024 Jan 12 |
Publication series
Name | AIAA SciTech Forum and Exposition, 2024 |
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Conference
Conference | AIAA SciTech Forum and Exposition, 2024 |
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Country/Territory | United States |
City | Orlando |
Period | 24/1/8 → 24/1/12 |
Bibliographical note
Publisher Copyright:© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
All Science Journal Classification (ASJC) codes
- Aerospace Engineering