NASA NTRS · 20080006009
Using the global positioning satellite system to determine attitude rates using doppler effects
Abstract
In the absence of a gyroscope, the attitude and attitude rate of a receiver can be determined using signals received by antennae on the receiver. Based on the signals received by the antennae, the Doppler difference between the signals is calculated. The Doppler difference may then be used to determine the attitude rate. With signals received from two signal sources by three antennae pairs, the three-dimensional attitude rate is determined.
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Campbell, Charles E.. 2003-07-15. Using the global positioning satellite system to determine attitude rates using doppler effects. https://ntrs.nasa.gov/citations/20080006009
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