Initial Dispersion Analysis and Midcourse Trajectory Correction Maneuver of Lunar Orbiter
Author:
Affiliation:
1. Korea Aerospace Research Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-5335
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Analysis on Delta-Vs to Maintain Extremely Low Altitude on the Moon and Its Application to CubeSat Mission;Journal of Astronomy and Space Sciences;2019-09
2. Initial Error Dispersion and Midcourse Correction Maneuver Analysis of the Lunar Orbiter;International Journal of Aeronautical and Space Sciences;2018-10-22
3. Flight Dynamics and Navigation for Planetary Missions in Korea: Past Efforts, Recent Status, and Future Preparations;Journal of Astronomy and Space Sciences;2018-09
4. Early Phase Contingency Trajectory Design for the Failure of the First Lunar Orbit Insertion Maneuver: Direct Recovery Options;Journal of Astronomy and Space Sciences;2017-12
5. Burn Delay Analysis of the Lunar Orbit Insertion for Korea Pathfinder Lunar Orbiter;Journal of Astronomy and Space Sciences;2017-12
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