The fifth monthly progress report includes corrections and additions to the previously submitted reports. The addition of the SRB propellant thickness as a state variable is included with the associated partial derivatives. During this reporting period, preliminary results of the estimation program checkout was presented to NASA technical personnel.
Space Shuttle Propulsion Parameter Estimation Using Optimal Estimation Techniques
1983
75 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Rocket Engines & Motors , Rocket Propellants , Data smoothing , Kalman filters , Solid rocket propellants , Space shuttle boosters , Acceleration (Physics) , Equations of motion , Ground support equipment , Moments of inertia , Prediction analysis techniques , Tracking (Position)
NTIS | 1994
NTRS | 1970
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