1. 1Systems, P.S. 2005. MANTA product description. http://www.psatellite.com/manta>.
2. 2Gim, D. & K. Alfriend. 2001. The state transition matrix of relative motion for the perturbed non-circular reference orbit. Proceedings 2001 AAS/AIAA Space Flight Mechanics Meeting, No. AAS 01-222, Santa Barbara, CA, February 2001.
3. 3Speyer, J.L. 2003. Computation and transmission requirements for a decentralized linear-quadratic Gaussian control problem. IEEE Trans. Automat. Contr. AC-24 April, 1979.
4. 4Busse, F. & J. How. 2002. Real-time experimental demonstration of precise decentralized relative navigation for formation flying spacecraft. AIAA Guidance, Navigation, and Control, Conference and Exhibit, Monterey, CA.
5. Real-Time Navigation of Formation-Flying Spacecraft Using Global-Positioning-System Measurements