TY - GEN
T1 - Autonomous integrated navigation using X-ray pulsars and asteroids
AU - Yang, Chengwei
AU - Gao, Dong
AU - Zheng, Jianhua
PY - 2012
Y1 - 2012
N2 - To improve the navigation performance of the spacecraft during interplanetary cruise, a novel integrated navigation system is proposed. For X-ray pulsar navigation (XNAV) is a hot and prospective research subject, and the optical navigation using asteroids is practical in space engineering, we designed an autonomous navigation system using one X-ray detector and one navigation camera. The measurement models of the XNAV based on the time difference of arrival and the optical navigation based on the images of asteroids are presented. To enhance practicality, the X-ray pulsars and asteroids are observed by turns. The batch least square filter, used by Deep Space I, is adopted to estimate the system state. The numerical simulation results show that the integrated navigation is feasible on the interplanetary cruise orbit. Moreover, compared with the XNAV and the optical navigation, the integrated navigation system can provide higher navigation performance.
AB - To improve the navigation performance of the spacecraft during interplanetary cruise, a novel integrated navigation system is proposed. For X-ray pulsar navigation (XNAV) is a hot and prospective research subject, and the optical navigation using asteroids is practical in space engineering, we designed an autonomous navigation system using one X-ray detector and one navigation camera. The measurement models of the XNAV based on the time difference of arrival and the optical navigation based on the images of asteroids are presented. To enhance practicality, the X-ray pulsars and asteroids are observed by turns. The batch least square filter, used by Deep Space I, is adopted to estimate the system state. The numerical simulation results show that the integrated navigation is feasible on the interplanetary cruise orbit. Moreover, compared with the XNAV and the optical navigation, the integrated navigation system can provide higher navigation performance.
UR - http://www.scopus.com/inward/record.url?scp=84883508480&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84883508480
SN - 9781622769797
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 3514
EP - 3518
BT - 63rd International Astronautical Congress 2012, IAC 2012
T2 - 63rd International Astronautical Congress 2012, IAC 2012
Y2 - 1 October 2012 through 5 October 2012
ER -