1. Vinh, N., Gilbert, E., Howe, R., Sheu, D., Lu, P. Reachable domain for interception at hyperbolic speeds. Acta Astronautica, 1995, 35 (1): 1–8.
2. Xue, D., Li, J., Baoyin, H. Study on reachable domain for satellite trajectory with coplanar impulse applied, Journal of Astronautics, 2009, 30(1): 88–92.
3. Xue, D., Li, J., Jiang, F. Reachable domain of a satellite with a coplanar impulse applied, Chinese Journal of Theoretical and Applied Mechanics, 2010, 42(2): 337–342.
4. Xue, D., Li, J., Baoyin, H., Jiang, F. Reachable domain for spacecraft with a single impulse. Journal of Guidance, Control, and Dynamics, 2010, 33(3): 934–942.
5. Li, X., He, X., Zhong, Q. Song, M. Reachable domain for satellite with two kinds of thrust. Acta Astronautica, 2011, 68(11-12): 1860–1864.