cheta.derived.pcad.DP_MAN_ANG

class cheta.derived.pcad.DP_MAN_ANG

Bases: DerivedParameterPcad

Maneuver Angle (Total) [deg]

Defined as the angle between the estimated quaternion and the target quaternion during a maneuver.

Computed using the fourth component of the delta quaternion between AOTARQT<N> and AOATTQT<N> when a maneuver is in progress (AOMANEND = NEND), otherwise equal to zero.

rootparams = ['aoattqt1', 'aoattqt2', 'aoattqt3', 'aoattqt4', 'aotarqt1', 'aotarqt2', 'aotarqt3', 'aomanend']

time_step = 1.025

dtype

calc(data)