A detailed development is presented of the psi-angle vector differential equation as applied to the error analysis of strapdown inertial navigation systems. The coordinate systems involved and the psi misalignment vector are clearly defined. It is proven that apart from a sign change the psi-angle differential equation in the error analysis of strapdown inertial navigation systems is identical to the one used in conventional gimbaled inertial navigation systems.
The Psi-Angle Error Equation in Strapdown Inertial Navigation Systems
IEEE Transactions on Aerospace and Electronic Systems ; AES-14 , 3 ; 539-542
1978-05-01
618240 byte
Article (Journal)
Electronic Resource
English
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