Date of Award
12-1991
Document Type
Thesis
Degree Name
Master of Science
Department
Department of Aeronautics and Astronautics
First Advisor
William E. Wiesel, PhD
Abstract
Previous work in the area of estimation of relative positions within a satellite cluster showed favorable results. However, the work was done using point mass orbits in the truth model. This thesis investigates the estimation of relative satellite positions operating in near circular orbit including the J2 term in Earth's geopotential. The iterated, extended Kalman filter is used as the on-board estimator in order to gain better performance in the face of the non-linearities. The dynamics in the estimator are based on the Clohessy- Wiltshire equations for relative orbital motion. Inputs to the host estimator are range measurements from each satellite in the cluster. The relative position to the host satellite is investigated. A comparison of the true error and the rms covariance was performed.
AFIT Designator
AFIT-GA-ENY-91D-5
DTIC Accession Number
ADA243897
Recommended Citation
Middendorf, J. Timothy, "Navigation of a Satellite Cluster with Realistic Dynamics" (1991). Theses and Dissertations. 7500.
https://scholar.afit.edu/etd/7500
Comments
The author's Vita page is omitted.