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Path: SC/Dynamics
% The right hand side of the wire equations formulated using Lagrange multipliers
2 2
The equations of motion are M d x/dt = Q
The constraints are phi = 0
If nIts > 0 it will use the iterative formulation.
Since version 2.
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Form:
xDot = WireC( x, t, s, mu, torque, force, penalty )
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Inputs
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x (m,1) The state vector
[x;v;q;w;xWire;vWire]
t (1,1) Time
s (:) Wire data structure
mu (1,1) Earth's gravitational constant
torque (3,1) External torque on core
force (3,1) External force on core
penalty (:) enalty function scalars [.alpha, .mu, .omega, .nIts]
nIts (1,1) Number of iterations
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Outputs
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xDot (:,1) The derivative of the state vector
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AerospaceUtils: Coord/QIToBDot Common: Quaternion/QForm Math: Linear/Cross Math: Linear/Mag Math: Linear/SkewSq Math: Linear/SkewSymm Math: Linear/Unit
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