Now showing items 1-2 of 2
Analysis of an Application where the Unscented Kalman Filter is not Appropriate
In this work a spin stabilized rocket with a ring of lateral pulse jets for attitude correction and fins that open early in flight is simulated. The rocket is simulated with five different sensor packages: rate gyros ...
Design, Testing, and Simulation of a Low-Cost, Light-Weight, Low-g IMU for the Navigation of an Indoor Blimp
In this thesis we develop an IMU for the purpose of navigating an autonomous indoor blimp. Due to the unique system properties of an indoor blimp, the developed IMU is light-weight and is capable of measuring slow rotational ...