A detailed analysis of space shuttle navigation for each of the major mission phases is presented. A covariance analysis program for prelaunch IMU calibration and alignment for the orbital flight tests (OFT) is described, and a partial error budget is presented. The ascent, orbital operations and deorbit maneuver study considered GPS-aided inertial navigation in the Phase III GPS (1984+) time frame. The entry and landing study evaluated navigation performance for the OFT baseline system. Detailed error budgets and sensitivity analyses are provided for both the ascent and entry studies.
Space shuttle navigation analysis
1976-09-10
Report
No indication
English
Space Shuttle Navigation Analysis
NTIS | 1976
|Space Shuttle navigation validation
AIAA | 1985
|Space Shuttle navigation validation
NTRS | 1985
|Space Shuttle Orbiter descent navigation
AIAA | 1982
|