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-rw-r--r--tests/core/math/test_quaternion.h50
1 files changed, 25 insertions, 25 deletions
diff --git a/tests/core/math/test_quaternion.h b/tests/core/math/test_quaternion.h
index 94eef6c463..1b80ffba0b 100644
--- a/tests/core/math/test_quaternion.h
+++ b/tests/core/math/test_quaternion.h
@@ -41,9 +41,9 @@
namespace TestQuaternion {
Quaternion quat_euler_yxz_deg(Vector3 angle) {
- double yaw = Math::deg2rad(angle[1]);
- double pitch = Math::deg2rad(angle[0]);
- double roll = Math::deg2rad(angle[2]);
+ double yaw = Math::deg_to_rad(angle[1]);
+ double pitch = Math::deg_to_rad(angle[0]);
+ double roll = Math::deg_to_rad(angle[2]);
// Generate YXZ (Z-then-X-then-Y) Quaternion using single-axis Euler
// constructor and quaternion product, both tested separately.
@@ -77,7 +77,7 @@ TEST_CASE("[Quaternion] Construct x,y,z,w") {
TEST_CASE("[Quaternion] Construct AxisAngle 1") {
// Easy to visualize: 120 deg about X-axis.
- Quaternion q(Vector3(1.0, 0.0, 0.0), Math::deg2rad(120.0));
+ Quaternion q(Vector3(1.0, 0.0, 0.0), Math::deg_to_rad(120.0));
// 0.866 isn't close enough; doctest::Approx doesn't cut much slack!
CHECK(q[0] == doctest::Approx(0.866025)); // Sine of half the angle.
@@ -88,7 +88,7 @@ TEST_CASE("[Quaternion] Construct AxisAngle 1") {
TEST_CASE("[Quaternion] Construct AxisAngle 2") {
// Easy to visualize: 30 deg about Y-axis.
- Quaternion q(Vector3(0.0, 1.0, 0.0), Math::deg2rad(30.0));
+ Quaternion q(Vector3(0.0, 1.0, 0.0), Math::deg_to_rad(30.0));
CHECK(q[0] == doctest::Approx(0.0));
CHECK(q[1] == doctest::Approx(0.258819)); // Sine of half the angle.
@@ -98,7 +98,7 @@ TEST_CASE("[Quaternion] Construct AxisAngle 2") {
TEST_CASE("[Quaternion] Construct AxisAngle 3") {
// Easy to visualize: 60 deg about Z-axis.
- Quaternion q(Vector3(0.0, 0.0, 1.0), Math::deg2rad(60.0));
+ Quaternion q(Vector3(0.0, 0.0, 1.0), Math::deg_to_rad(60.0));
CHECK(q[0] == doctest::Approx(0.0));
CHECK(q[1] == doctest::Approx(0.0));
@@ -109,7 +109,7 @@ TEST_CASE("[Quaternion] Construct AxisAngle 3") {
TEST_CASE("[Quaternion] Construct AxisAngle 4") {
// More complex & hard to visualize, so test w/ data from online calculator.
Vector3 axis(1.0, 2.0, 0.5);
- Quaternion q(axis.normalized(), Math::deg2rad(35.0));
+ Quaternion q(axis.normalized(), Math::deg_to_rad(35.0));
CHECK(q[0] == doctest::Approx(0.131239));
CHECK(q[1] == doctest::Approx(0.262478));
@@ -119,7 +119,7 @@ TEST_CASE("[Quaternion] Construct AxisAngle 4") {
TEST_CASE("[Quaternion] Construct from Quaternion") {
Vector3 axis(1.0, 2.0, 0.5);
- Quaternion q_src(axis.normalized(), Math::deg2rad(35.0));
+ Quaternion q_src(axis.normalized(), Math::deg_to_rad(35.0));
Quaternion q(q_src);
CHECK(q[0] == doctest::Approx(0.131239));
@@ -129,9 +129,9 @@ TEST_CASE("[Quaternion] Construct from Quaternion") {
}
TEST_CASE("[Quaternion] Construct Euler SingleAxis") {
- double yaw = Math::deg2rad(45.0);
- double pitch = Math::deg2rad(30.0);
- double roll = Math::deg2rad(10.0);
+ double yaw = Math::deg_to_rad(45.0);
+ double pitch = Math::deg_to_rad(30.0);
+ double roll = Math::deg_to_rad(10.0);
Vector3 euler_y(0.0, yaw, 0.0);
Quaternion q_y(euler_y);
@@ -156,9 +156,9 @@ TEST_CASE("[Quaternion] Construct Euler SingleAxis") {
}
TEST_CASE("[Quaternion] Construct Euler YXZ dynamic axes") {
- double yaw = Math::deg2rad(45.0);
- double pitch = Math::deg2rad(30.0);
- double roll = Math::deg2rad(10.0);
+ double yaw = Math::deg_to_rad(45.0);
+ double pitch = Math::deg_to_rad(30.0);
+ double roll = Math::deg_to_rad(10.0);
// Generate YXZ comparision data (Z-then-X-then-Y) using single-axis Euler
// constructor and quaternion product, both tested separately.
@@ -187,9 +187,9 @@ TEST_CASE("[Quaternion] Construct Euler YXZ dynamic axes") {
}
TEST_CASE("[Quaternion] Construct Basis Euler") {
- double yaw = Math::deg2rad(45.0);
- double pitch = Math::deg2rad(30.0);
- double roll = Math::deg2rad(10.0);
+ double yaw = Math::deg_to_rad(45.0);
+ double pitch = Math::deg_to_rad(30.0);
+ double roll = Math::deg_to_rad(10.0);
Vector3 euler_yxz(pitch, yaw, roll);
Quaternion q_yxz(euler_yxz);
Basis basis_axes(euler_yxz);
@@ -199,7 +199,7 @@ TEST_CASE("[Quaternion] Construct Basis Euler") {
TEST_CASE("[Quaternion] Construct Basis Axes") {
// Arbitrary Euler angles.
- Vector3 euler_yxz(Math::deg2rad(31.41), Math::deg2rad(-49.16), Math::deg2rad(12.34));
+ Vector3 euler_yxz(Math::deg_to_rad(31.41), Math::deg_to_rad(-49.16), Math::deg_to_rad(12.34));
// Basis vectors from online calculation of rotation matrix.
Vector3 i_unit(0.5545787, 0.1823950, 0.8118957);
Vector3 j_unit(-0.5249245, 0.8337420, 0.1712555);
@@ -248,9 +248,9 @@ TEST_CASE("[Quaternion] Product (book)") {
}
TEST_CASE("[Quaternion] Product") {
- double yaw = Math::deg2rad(45.0);
- double pitch = Math::deg2rad(30.0);
- double roll = Math::deg2rad(10.0);
+ double yaw = Math::deg_to_rad(45.0);
+ double pitch = Math::deg_to_rad(30.0);
+ double roll = Math::deg_to_rad(10.0);
Vector3 euler_y(0.0, yaw, 0.0);
Quaternion q_y(euler_y);
@@ -292,7 +292,7 @@ TEST_CASE("[Quaternion] Product") {
TEST_CASE("[Quaternion] xform unit vectors") {
// Easy to visualize: 120 deg about X-axis.
// Transform the i, j, & k unit vectors.
- Quaternion q(Vector3(1.0, 0.0, 0.0), Math::deg2rad(120.0));
+ Quaternion q(Vector3(1.0, 0.0, 0.0), Math::deg_to_rad(120.0));
Vector3 i_t = q.xform(Vector3(1.0, 0.0, 0.0));
Vector3 j_t = q.xform(Vector3(0.0, 1.0, 0.0));
Vector3 k_t = q.xform(Vector3(0.0, 0.0, 1.0));
@@ -305,7 +305,7 @@ TEST_CASE("[Quaternion] xform unit vectors") {
CHECK(k_t.length_squared() == doctest::Approx(1.0));
// Easy to visualize: 30 deg about Y-axis.
- q = Quaternion(Vector3(0.0, 1.0, 0.0), Math::deg2rad(30.0));
+ q = Quaternion(Vector3(0.0, 1.0, 0.0), Math::deg_to_rad(30.0));
i_t = q.xform(Vector3(1.0, 0.0, 0.0));
j_t = q.xform(Vector3(0.0, 1.0, 0.0));
k_t = q.xform(Vector3(0.0, 0.0, 1.0));
@@ -318,7 +318,7 @@ TEST_CASE("[Quaternion] xform unit vectors") {
CHECK(k_t.length_squared() == doctest::Approx(1.0));
// Easy to visualize: 60 deg about Z-axis.
- q = Quaternion(Vector3(0.0, 0.0, 1.0), Math::deg2rad(60.0));
+ q = Quaternion(Vector3(0.0, 0.0, 1.0), Math::deg_to_rad(60.0));
i_t = q.xform(Vector3(1.0, 0.0, 0.0));
j_t = q.xform(Vector3(0.0, 1.0, 0.0));
k_t = q.xform(Vector3(0.0, 0.0, 1.0));
@@ -333,7 +333,7 @@ TEST_CASE("[Quaternion] xform unit vectors") {
TEST_CASE("[Quaternion] xform vector") {
// Arbitrary quaternion rotates an arbitrary vector.
- Vector3 euler_yzx(Math::deg2rad(31.41), Math::deg2rad(-49.16), Math::deg2rad(12.34));
+ Vector3 euler_yzx(Math::deg_to_rad(31.41), Math::deg_to_rad(-49.16), Math::deg_to_rad(12.34));
Basis basis_axes(euler_yzx);
Quaternion q(basis_axes);
generated by cgit v1.2.3 (git 2.25.1) at 2024-11-22 04:02:42 +0000