Hardware-In-The-Loop Testing of Continuous Control Algorithms for a Precision Formation Flying Demonstration Mission
暂无分享,去创建一个
John Higinbotham | Bo J. Naasz | David Gaylor | Richard Burns | D. Gaylor | R. Burns | B. Naasz | J. Higinbotham
[1] Derek F Lawden,et al. Optimal trajectories for space navigation , 1964 .
[2] J. How,et al. Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits , 2000 .
[3] H. Schaub,et al. J2 Invariant Relative Orbits for Spacecraft Formations , 2001 .
[4] C. Sabol,et al. Satellite Formation Flying Design and Evolution , 2001 .
[5] J. Leitner,et al. A hardware-in-the-loop testbed for spacecraft formation flying applications , 2001, 2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542).
[6] S. Vadali,et al. CONTROL OF SATELLITE FORMATIONS , 2001 .
[7] E. Glenn Lightsey,et al. A real-time kinematic GPS sensor for spacecraft relative navigation Ein GPS Sensor zur kinematischen Relativnavigation von Raumfahrzeugen in Echtzeit , 2002 .
[8] E. Gill,et al. First Results from a Hardware-in-the-Loop Demonstration of Closed-Loop Autonomous Formation Flying , 2003 .
[9] Randal W. Beard,et al. A decentralized scheme for spacecraft formation flying via the virtual structure approach , 2003, Proceedings of the 2003 American Control Conference, 2003..
[10] Jonathan P. How,et al. Distributed coordination and control of formation flying spacecraft , 2003, Proceedings of the 2003 American Control Conference, 2003..
[11] R. Burns,et al. Development of a crosslink channel simulator , 2004, 2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720).