Modeling, dynamics and control of spacecraft relative motion in a perturbed keplerian orbit

• المؤلفون الرئيسيون: Okasha, Mohamed Elsayed Aly Abd Elaziz, Newman, Brett
• التنسيق: مقال
• اللغة: English; English
• منشور في: The Korean Society for Aeronautical & Space Sciences 2015
• الموضوعات: TL500 Aeronautics; TL787 Astronautics
• الوصول للمادة أونلاين: http://irep.iium.edu.my/42772/1/8%2877-88%2914-064.pdf; http://irep.iium.edu.my/42772/4/42772-_wos%2Cscopus.pdf; http://irep.iium.edu.my/42772/; http://ijass.org/On_line/admin/files/8(77~88)14-064.pdf; http://dx.doi.org/10.5139/IJASS.2015.16.1.77

The dynamics of relative motion in a perturbed orbital environment are exploited based on Gauss’ and Cowell’s variational equations. The inertial coordinate frame and relative coordinate frame (Hill frame) are used, and a linear high fidelity model is developed to describe the relative motion. This...