A navigation system for the entry phase of a Space Shuttle mission which is an aided-inertial system which uses a Kalman filter to mix IMU data with data derived from external navigation aids is evaluated. A drag pseudo-measurement used during radio blackout is treated as an additional external aid. A comprehensive truth model with 101 states is formulated and used to generate detailed error budgets at several significant time points -- end-of-blackout, start of final approach, over runway...
Topics: NASA Technical Reports Server (NTRS), ATMOSPHERIC ENTRY, INERTIAL NAVIGATION, LANDING AIDS, SPACE...
The lateral approach is presented for proximity operations associated with the retrieval of free flying payloads. An out of plane final approach emphasizing onboard software support is recommended for all except the latter segment of the final approach in which manual control is considered mandatory. An overall assessment of various candidate proximity operations techniques are made.
Topics: NASA Technical Reports Server (NTRS), LATERAL CONTROL, PAYLOADS, SPACE SHUTTLE ORBITERS, COMPUTER...
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....
Topics: NASA Technical Reports Server (NTRS), COVARIANCE, ORBITAL MANEUVERS, SPACE NAVIGATION, SPACE...
Studies related to the baseline navigation system for the orbiter are presented. The baseline navigation system studies include a covariance analysis of the Inertial Measurement Unit calibration and alignment procedures, postflight IMU error recovery for the approach and landing phases, on-orbit calibration of IMU instrument biases, and a covariance analysis of entry and prelaunch navigation system performance.
Topics: NASA Technical Reports Server (NTRS), AVIONICS, COVARIANCE, INERTIAL PLATFORMS, NAVIGATION AIDS,...
