Date of Award
4-2016
Degree Type
Thesis
Degree Name
Master of Science in Aeronautics and Astronautics
Department
Aeronautics and Astronautics
First Advisor
Inseok Hwang
Committee Chair
Inseok Hwang
Committee Member 1
Carolin E. Frueh
Committee Member 2
Dengfeng Sun
Abstract
In order to efficiently maintain space situational awareness, care must be taken to optimally allocate expensive observation resources. In most situations the available sensors capable of tracking spacecraft have their time split between many different monitoring responsibilities. Tracking maneuvering spacecraft can be especially difficult as the schedule of maneuvers may not be known and will often throw off previous orbital models. Effectively solving this tasking problem is an ongoing focus of research in the area of space situational awareness. Most methods of automated tasking do not make use of interacting multiple model extended Kalman filter techniques to better track satellites during maneuvers. This paper proposes a modification to a Fisher information gain and estimated state covariance based sensor tasking method to take maneuver probability and multiple model dynamics into account. By incorporating the probabilistic maneuvering model, sensor tasking can be improved during satellite maneuvers using constrained resources. The proposed methods are verified through the use of numerical simulations with multiple maneuvering satellites and both orbital and ground-based sensors.
Recommended Citation
Lace, Arthur A., "Dynamic sensor tasking and IMM EKF estimation for tracking impulsively maneuvering satellites" (2016). Open Access Theses. 784.
https://docs.lib.purdue.edu/open_access_theses/784