Attitude determination for a strapdown inertial system using the Euler axis/angle and quaternion parameters
- 16 August 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- A New Mathematical Formulation for Strapdown Inertial NavigationIEEE Transactions on Aerospace and Electronic Systems, 1971
- Derivation of the quaternion scheme via the Euler axis and angleJournal of Spacecraft and Rockets, 1970
- A NEW SECOND-ORDER SOLUTION FOR STRAPPED-DOWN ATTITUDE COMPUTATIONPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966