TY - JOUR
T1 - Pseudolite-based multiple space-vehicles relative navigation for formation flying
AU - Yue, Xiaokui
AU - Yuan, Jianping
PY - 2005
Y1 - 2005
N2 - Precise relative navigation is a necessary and important technology for any operation of multiple space vehicles on-orbit formation flying together. Carrier-phase Differential GPS (CDGPS) positioning has been proven to be an accurate technique for relative positioning and attitude determining between multiple vehicles. But, the present satellite navigation system has no enough covering performance for some flying missions. For example, in high orbits, navigation satellite reception is often not sufficient to resolve position and attitude between all vehicles in the formation flying. One of the methods of taking advantage of satellite navigation system in such cases is to augment the available signals with additional signals from pseudolites. In fact, pseudolite is just a special transmitter, whose signals have many of the characteristics of the signals broadcast by the satellites of navigation system. Meanwhile, pseudolite can be placed on the ground, or in the MEO or GEO orbits. In this paper, an onboard pseudolite augmentation system of each vehicle for formation flying is studied, such as each vehicle can exchange navigation data with other vehicles. Such augmentation system can be used to improve the performance of satellite navigation system, e.g. GPS, GLONASS, and so on. Based on the correlative studies, some conclusion for the space application of pseudolite is given, including some idea about the arrangement of correlative ground experiments.
AB - Precise relative navigation is a necessary and important technology for any operation of multiple space vehicles on-orbit formation flying together. Carrier-phase Differential GPS (CDGPS) positioning has been proven to be an accurate technique for relative positioning and attitude determining between multiple vehicles. But, the present satellite navigation system has no enough covering performance for some flying missions. For example, in high orbits, navigation satellite reception is often not sufficient to resolve position and attitude between all vehicles in the formation flying. One of the methods of taking advantage of satellite navigation system in such cases is to augment the available signals with additional signals from pseudolites. In fact, pseudolite is just a special transmitter, whose signals have many of the characteristics of the signals broadcast by the satellites of navigation system. Meanwhile, pseudolite can be placed on the ground, or in the MEO or GEO orbits. In this paper, an onboard pseudolite augmentation system of each vehicle for formation flying is studied, such as each vehicle can exchange navigation data with other vehicles. Such augmentation system can be used to improve the performance of satellite navigation system, e.g. GPS, GLONASS, and so on. Based on the correlative studies, some conclusion for the space application of pseudolite is given, including some idea about the arrangement of correlative ground experiments.
KW - Formation flying
KW - GPS
KW - Pseudolite
KW - Relative navigation
UR - http://www.scopus.com/inward/record.url?scp=33644518233&partnerID=8YFLogxK
U2 - 10.1117/12.658257
DO - 10.1117/12.658257
M3 - 会议文章
AN - SCOPUS:33644518233
SN - 0277-786X
VL - 5985 PART II
JO - Proceedings of SPIE - The International Society for Optical Engineering
JF - Proceedings of SPIE - The International Society for Optical Engineering
M1 - 598543
T2 - International Conference on Space Information Technology
Y2 - 19 November 2005 through 20 November 2005
ER -