Formalized Approach to Obtaining Optimal Coefficients for Coning Algorithms
- 1 January 1999
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 22 (1), 165-168
- https://doi.org/10.2514/2.7620
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Analysis of the Frequency, Damping, and Total Insensitivities of Input Shaping DesignsJournal of Guidance, Control, and Dynamics, 1997
- Vibration Reduction Using Multi-Hump Input ShapersJournal of Dynamic Systems, Measurement, and Control, 1997
- Efficient class of optimized coning compensation algorithmsJournal of Guidance, Control, and Dynamics, 1996
- Improved strapdown coning algorithmsIEEE Transactions on Aerospace and Electronic Systems, 1992
- On the rotation vector differential equationIEEE Transactions on Aerospace and Electronic Systems, 1991
- Extension of strapdown attitude algorithm for high-frequency base motionJournal of Guidance, Control, and Dynamics, 1990
- Preshaping Command Inputs to Reduce System VibrationJournal of Dynamic Systems, Measurement, and Control, 1990
- A new strapdown attitude algorithmJournal of Guidance, Control, and Dynamics, 1983
- A New Mathematical Formulation for Strapdown Inertial NavigationIEEE Transactions on Aerospace and Electronic Systems, 1971
- A New Algorithm for Strapped-Down Inertial NavigationIEEE Transactions on Aerospace and Electronic Systems, 1967