Covariance-Based Multiple-Impulse Rendezvous Design
نویسندگان
چکیده
منابع مشابه
Optimal Two-Impulse Rendezvous Using Multiple-Revolution Lambert Solutions
Theminimum-¢V, xed-time, two-impulse rendezvousbetween two spacecraft orbitingalong two coplanarunidirectional circular orbits (moving-target rendezvous) is studied. To reach this goal, the minimum-¢V, xed-time, two-impulse transfer problem between two xed points on two circular orbits is rst solved. This xed-endpoint transfer is related to the moving-target rendezvous problemby a sim...
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ژورنال
عنوان ژورنال: IEEE Transactions on Aerospace and Electronic Systems
سال: 2019
ISSN: 0018-9251,1557-9603,2371-9877
DOI: 10.1109/taes.2018.2882939