|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: Math/AStar
% Compute the angle change needed to change a trajectory so that it
passes through the second right ascension and declination.
Type DeltaAngleForNewRADec for demo.
--------------------------------------------------------------------------
Form:
DeltaAngleForNewRADec;
deltaAngle = DeltaAngleForNewRADec( v1, rA1, dec1, rA2, dec2 )
--------------------------------------------------------------------------
------
Inputs
------
v1 (3,1) Current velocity vector
rA1 (1,1) Current right ascension (rad)
dec1 (1,1) Current declination (rad)
rA2 (1,1) New right ascension (rad)
dec2 (1,1) New declination
-------
Outputs
-------
deltaAngle (1,1) Velocity vector angle change (rad)
--------------------------------------------------------------------------
Common: Transform/RaDec2U Math: Linear/Cross Math: Linear/Dot Math: Linear/Unit
Back to the Math Module page