Title :
A new kinematic theorem for rotational motion
Author :
Blankinship, Kevin
Author_Institution :
Navigation Syst. Group, Boeing Integrated Defense Syst., Midwest City, OK, USA
Abstract :
The Goodman-Robinson theorem (ASME Jour. of App. Mech., vol.25, p, 210-213, 1968), used to explain kinematic drift in strapdown attitude algorithms due to coning motion, can be thought of as an integral form of the rotation vector differential equation. This theorem states that, in the absence of instrument errors, the delta-theta count of a rate-integrating-type gyro is equal to the time integral of the angular velocity component along the gyro sensitive axis, plus the area that the sensitive axis traces out on a sphere of unit radius. This paper utilizes the Darboux frame from differential geometry to obtain an expression for the area term in the Goodman-Robinson formula. It turns out that this term is equal to the time integral of the component along the gyro sensitive axis of the angular velocity of the angular velocity of the sensitive axis, plus exterior angle terms. The results of this paper provide a geometric explanation of how movement of the direction of the angular velocity vector contributes to kinematic drift.
Keywords :
angular velocity measurement; attitude measurement; differential geometry; gyroscopes; kinematics; rotation measurement; Goodman-Robinson theorem; angular velocity vector; coning motion; differential geometry Darboux frame; gyro delta-theta count; gyro sensitive axis angular velocity component; kinematic drift; rate-integrating-type gyro; rotation vector differential equation; rotational motion kinematic theorem; strapdown attitude algorithms; Angular velocity; Cities and towns; Differential equations; Geometry; Gyroscopes; History; Instruments; Integral equations; Kinematics; Navigation;
Conference_Titel :
Position Location and Navigation Symposium, 2004. PLANS 2004
Print_ISBN :
0-7803-8416-4
DOI :
10.1109/PLANS.2004.1309007