Initial attitude determination and correction of gyro-free INS angular orientation on the basis of GPS linear navigation parameters
Authors:
- A.A. SolovievASA.A. Soloviev
- T.-K.J. KooTKT.-K.J. Koo
- 1 January 1997
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 1034-1039
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Gyroscope free strapdown inertial measurement unit by six linear accelerometersJournal of Guidance, Control, and Dynamics, 1994
- Recursive Attitude Determination from Vector Observations: Direction Cosine Matrix IdentificationJournal of Guidance, Control, and Dynamics, 1984