Spacecraft Attitude Determination And Control

By M. Hartmann. 2016

392 citations recorded by the source corpus.

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

Linear Quaternion Differential Equations: Basic Theory and Fundamental Results (2015, background): “Wertz [40] derived the general attitude motion equations for the quaternions assuming a constant rotation rate over an infinitesimal time ∆t such that qk+1 = qk + q̇∆t where q = (q1, q2, q3, q4) T , and the quaternion differentiated with respect to time is approximated by q̇ = 1 2 Ω · qk with the sk”