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.
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Form:
DeltaAngleForNewRADec;
deltaAngle = DeltaAngleForNewRADec( v1, rA1, dec1, rA2, dec2 )
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Inputs
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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
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Outputs
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deltaAngle (1,1) Velocity vector angle change (rad)
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Common: Transform/RaDec2U Math: Linear/Cross Math: Linear/Dot Math: Linear/Unit
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