
International Journal of Space Science and Engineering
2016 Vol.4 No.2
Pages | Title and author(s) |
77-90 | Guaranteed ellipsoidal estimation for satellite formation flying collision avoidanceG. Vukovich; Y. Kim DOI: 10.1504/IJSPACESE.2016.081560 |
91-105 | Tether deployment with in-plane angular and explicit velocity constraints by barrier Lyapunov functionMing Liu; Xingqun Zhan; Bing Zhu DOI: 10.1504/IJSPACESE.2016.081562 |
106-120 | Orbital design and optimal control of cislunar transport mission using spinning tether systemHong-Shi Lu; Chang-Qing Wang; Ai-Jun Li; Zabolotnov Yuriy DOI: 10.1504/IJSPACESE.2016.081567 |
121-137 | Post Newtonian gravity, a new simpler approachH. Ron Harrison DOI: 10.1504/IJSPACESE.2016.081569 |
138-165 | Optimal control of satellite formations due to oblateness perturbationsF.A. Abd El-Salam DOI: 10.1504/IJSPACESE.2016.081571 |