TY - GEN
T1 - Pose tracking of a noncooperative spacecraft during docking maneuvers using a time-of-flight sensor
AU - Ventura, Jacopo
AU - Fleischner, Andreas
AU - Walter, Ulrich
N1 - Publisher Copyright:
© 2016 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - This paper presents a pose estimation procedure for tracking attitude and position of a noncooperative tumbling spacecraft during rendezvous and docking maneuvers. The key aspect of the method is that the current state of the target spacecraft is estimated in real-time using a low-resolution depth-image of the scene and a known model of the vehicle. The proposed procedure exploits the iterative closest point algorithm implemented in closed-loop fashion. In order to guarantee stability of the solution, the current pose of the target is predicted onboard by propagating the last estimated state using a dedicated dynamics model of the maneuver. The tracking procedure is initialized with a fast template matching algorithm that determines attitude and position of the target without prior information on its state. The capabilities of the proposed procedure are demonstrated using a full degreesof- freedom hardware simulator. In these experiments, the Microsoft Kinect v2 sensor is employed for real-time acquisition of the target spacecraft depth image. The results demonstrate the effectiveness of the proposed procedure during docking maneuvers to a noncooperative tumbling target. However, prediction of the current target pose is crucial for algorithm robustness.
AB - This paper presents a pose estimation procedure for tracking attitude and position of a noncooperative tumbling spacecraft during rendezvous and docking maneuvers. The key aspect of the method is that the current state of the target spacecraft is estimated in real-time using a low-resolution depth-image of the scene and a known model of the vehicle. The proposed procedure exploits the iterative closest point algorithm implemented in closed-loop fashion. In order to guarantee stability of the solution, the current pose of the target is predicted onboard by propagating the last estimated state using a dedicated dynamics model of the maneuver. The tracking procedure is initialized with a fast template matching algorithm that determines attitude and position of the target without prior information on its state. The capabilities of the proposed procedure are demonstrated using a full degreesof- freedom hardware simulator. In these experiments, the Microsoft Kinect v2 sensor is employed for real-time acquisition of the target spacecraft depth image. The results demonstrate the effectiveness of the proposed procedure during docking maneuvers to a noncooperative tumbling target. However, prediction of the current target pose is crucial for algorithm robustness.
UR - http://www.scopus.com/inward/record.url?scp=85088352522&partnerID=8YFLogxK
U2 - 10.2514/6.2016-0875
DO - 10.2514/6.2016-0875
M3 - Conference contribution
AN - SCOPUS:85088352522
SN - 9781624103896
T3 - 2016 AIAA Guidance, Navigation, and Control Conference
BT - AIAA Guidance, Navigation, and Control Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Guidance, Navigation, and Control Conference, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -