An error analysis of an inertial navigator leads to the set of normalized state
Chapter 7, Problem 7.46(choose chapter or problem)
An error analysis of an inertial navigator leads to the set of normalized state equations where X1 = eastvelocity error, X2 = platform tilt about the north axis, X3 = northgyro drift, u = gyro drift rate of change. Design a reduced-order estimator with y = X1 as the measurement, and place the observer-error poles at 0.1 and 0.1. Be sure to provide all the relevant estimator equations.
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