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-rw-r--r--logic/simple-mat.cpp96
1 files changed, 0 insertions, 96 deletions
diff --git a/logic/simple-mat.cpp b/logic/simple-mat.cpp
deleted file mode 100644
index 57571f9e..00000000
--- a/logic/simple-mat.cpp
+++ /dev/null
@@ -1,96 +0,0 @@
-#include "simple-mat.hpp"
-#include <cmath>
-
-namespace euler {
-
-euler_t OPENTRACK_LOGIC_EXPORT rmat_to_euler(const rmat& R)
-{
- using std::atan2;
- using std::sqrt;
-
- const double cy = sqrt(R(2,2)*R(2, 2) + R(2, 1)*R(2, 1));
- const bool large_enough = cy > 1e-10;
- if (large_enough)
- return euler_t(atan2(-R(1, 0), R(0, 0)),
- atan2(R(2, 0), cy),
- atan2(-R(2, 1), R(2, 2)));
- else
- return euler_t(atan2(R(0, 1), R(1, 1)),
- atan2(R(2, 0), cy),
- 0);
-}
-
-// tait-bryan angles, not euler
-rmat OPENTRACK_LOGIC_EXPORT euler_to_rmat(const euler_t& input)
-{
- const double H = -input(0);
- const double P = -input(1);
- const double B = -input(2);
-
- using std::cos;
- using std::sin;
-
- const auto c1 = cos(H);
- const auto s1 = sin(H);
- const auto c2 = cos(P);
- const auto s2 = sin(P);
- const auto c3 = cos(B);
- const auto s3 = sin(B);
-
- return rmat(
- // z
- c1 * c2,
- c1 * s2 * s3 - c3 * s1,
- s1 * s3 + c1 * c3 * s2,
- // y
- c2 * s1,
- c1 * c3 + s1 * s2 * s3,
- c3 * s1 * s2 - c1 * s3,
- // x
- -s2,
- c2 * s3,
- c2 * c3
- );
-}
-
-// https://en.wikipedia.org/wiki/Davenport_chained_rotations#Tait.E2.80.93Bryan_chained_rotations
-void OPENTRACK_LOGIC_EXPORT tait_bryan_to_matrices(const euler_t& input,
- rmat& r_roll,
- rmat& r_pitch,
- rmat& r_yaw)
-{
- using std::cos;
- using std::sin;
-
- {
- const double phi = -input(2);
- const double sin_phi = sin(phi);
- const double cos_phi = cos(phi);
-
- r_roll = rmat(1, 0, 0,
- 0, cos_phi, -sin_phi,
- 0, sin_phi, cos_phi);
- }
-
- {
- const double theta = input(1);
- const double sin_theta = sin(theta);
- const double cos_theta = cos(theta);
-
- r_pitch = rmat(cos_theta, 0, -sin_theta,
- 0, 1, 0,
- sin_theta, 0, cos_theta);
- }
-
- {
- const double psi = -input(0);
- const double sin_psi = sin(psi);
- const double cos_psi = cos(psi);
-
- r_yaw = rmat(cos_psi, -sin_psi, 0,
- sin_psi, cos_psi, 0,
- 0, 0, 1);
- }
-}
-
-} // end ns euler