Title :
Improved strapdown coning algorithms
Author :
Jiang, Yeon Fuh ; Lin, Yu Ping
Author_Institution :
Nat. Chiao Tung Univ., Hsinchu, Taiwan
fDate :
4/1/1992 12:00:00 AM
Abstract :
Three improved algorithms for strapdown attitude computation utilizing accumulated gyro increments from the previous and current update are developed and evaluated analytically under classical coning motion. The error criterion of Miller is derived directly from the rotation vector concept. The accuracy of updating rotation vector estimation can be improved at least two orders of magnitude as compared with those of conventional algorithms. The proposed algorithm is equivalent to increasing the number of gyro samples used in the conventional method and it requires less computer loading
Keywords :
aerospace computing; computerised navigation; computerised signal processing; error analysis; gyroscopes; inertial navigation; Miller; accumulated gyro increments; coning motion; error criterion; rotation vector; strapdown coning algorithms; Algorithm design and analysis; Artificial intelligence; Attitude control; Computer errors; Control engineering; Differential equations; Error correction; Motion analysis; Quaternions; Vehicles;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on