Application of GPS for Missile Post Flight Guidance Accuracy Analysis
Document Type
Conference Proceeding
Publication Date
5-1993
Publication Title
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
Abstract
The high quality of a GPS-based trajectory reference makes it useful for evaluating the performance of a missile's Interial Navigation System (INS) during a missile flight test. The complexity of the design of the GPS user segment depends on flight test objectives and factors such as the expected satellite/vehicle geometry. Design curves are developed which illustrate the relationship between flight test objectives, the GPS user segment design, and such factors as antenna performance.
Repository Citation
Dougherty, John J.; Simon, Daniel J.; and El-Sherief, Hossny, "Application of GPS for Missile Post Flight Guidance Accuracy Analysis" (1993). Electrical and Computer Engineering Faculty Publications. 178.
https://engagedscholarship.csuohio.edu/enece_facpub/178
Original Citation
J. Dougherty, H. El-Sherief and D. Simon. (1993). Application of GPS for Missile Post Flight Guidance Accuracy Analysis. IEEE Conference on Aerospace Control Systems, 1678-1685, doi: 10.1109/AEROCS.1993.721039.
DOI
10.1109/AEROCS.1993.721039
