TY - JOUR
T1 - A rapid maneuver path planning method with complex sensor pointing constraints in the attitude space
AU - Xu, Rui
AU - Wu, Changqing
AU - Zhu, Shengying
AU - Fang, Baodong
AU - Wang, Wei
AU - Xu, Lida
AU - He, Wu
N1 - Publisher Copyright:
© 2016, Springer Science+Business Media New York.
PY - 2017/8/1
Y1 - 2017/8/1
N2 - Large-scale and high-resolution perception is easy to achieve for the physical world, if satellite technology was used in Internet of Things (IoT) in the future. Remote sensing satellite is superior to original method for ground target detection and environmental perception, which could be completed through onboard perception sensors. In the process of detection and perception, satellite needs to frequently perform attitude maneuver in order to meet a variety of task requirements. We have to face with multi-object, multi-sensors constrained maneuver problem. Not only the kinematic and dynamics constraints should been taken into account, but the engineering bounded constraints need to be considered. Moreover, sensor pointing constraints should be elaborated and analyzed reasonably. It is increasingly important how to achieve attitude maneuver in these complex constraints safely and rapidly. Firstly, sensor pointing constraints are translated to quadratic form in order to simplify the representation and computation in the attitude quaternion space. Secondly, we propose an improved RRT planning algorithm for spacecraft, which is able to address a variety of sensor pointing constraints. This algorithm will be used as a global planner, in which the uniformly distributed nodes in the expansion space are randomly sampled and the expanded nodes are screened out based on the comparative evaluation function. Finally, simulation results validate the advantages of the proposed algorithm.
AB - Large-scale and high-resolution perception is easy to achieve for the physical world, if satellite technology was used in Internet of Things (IoT) in the future. Remote sensing satellite is superior to original method for ground target detection and environmental perception, which could be completed through onboard perception sensors. In the process of detection and perception, satellite needs to frequently perform attitude maneuver in order to meet a variety of task requirements. We have to face with multi-object, multi-sensors constrained maneuver problem. Not only the kinematic and dynamics constraints should been taken into account, but the engineering bounded constraints need to be considered. Moreover, sensor pointing constraints should be elaborated and analyzed reasonably. It is increasingly important how to achieve attitude maneuver in these complex constraints safely and rapidly. Firstly, sensor pointing constraints are translated to quadratic form in order to simplify the representation and computation in the attitude quaternion space. Secondly, we propose an improved RRT planning algorithm for spacecraft, which is able to address a variety of sensor pointing constraints. This algorithm will be used as a global planner, in which the uniformly distributed nodes in the expansion space are randomly sampled and the expanded nodes are screened out based on the comparative evaluation function. Finally, simulation results validate the advantages of the proposed algorithm.
KW - Industrial information integration
KW - Internet of Things
KW - Path planning
KW - Pointing constraints
KW - RRT
KW - Remote sensing satellite
UR - http://www.scopus.com/inward/record.url?scp=84961859351&partnerID=8YFLogxK
U2 - 10.1007/s10796-016-9642-1
DO - 10.1007/s10796-016-9642-1
M3 - Article
AN - SCOPUS:84961859351
SN - 1387-3326
VL - 19
SP - 945
EP - 953
JO - Information Systems Frontiers
JF - Information Systems Frontiers
IS - 4
ER -