State space techniques for obtaining math models of flight test vehicles with nonlinear measurement variables in many different moving bases are presented. Inertial measurement units (IMU on-board variables are related to the state variables of interest for obtaining a Best Estimate of Trajectory (BET). (Author)
State Space Techniques for Inertial Measurement Unit Variables for Range Tests
1972
140 pages
Report
Keine Angabe
Englisch
Spacecraft Trajectories & Flight Mechanics , Missile Trajectories & Reentry Dynamics , Navigation & Guidance System Components , Range finding , Guided missile trajectories , Rocket trajectories , Mathematical prediction , Inertial guidance , Random variables , Guided missile ranges , Launch vehicles(Aerospace) , Vector analysis , Nonlinear systems , Stabilized platforms , Velocity , Mathematical models , Control theory , State space method , Computer aided analysis
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