diff --git a/include/cglm/euler.h b/include/cglm/euler.h
index fb4adc0..d069f10 100644
--- a/include/cglm/euler.h
+++ b/include/cglm/euler.h
@@ -43,7 +43,46 @@
 
 #include "common.h"
 
-#include "handed/euler_to_quat_rh.h"
+#ifdef CGLM_FORCE_LEFT_HANDED
+#  include "handed/euler_to_quat_lh.h"
+#else
+#  include "handed/euler_to_quat_rh.h"
+#endif
+
+
+#ifndef CGLM_CLIPSPACE_INCLUDE_ALL
+#  if CGLM_CONFIG_CLIP_CONTROL == CGLM_CLIP_CONTROL_LH_ZO
+#    include "clipspace/ortho_lh_zo.h"
+#    include "clipspace/persp_lh_zo.h"
+#    include "clipspace/view_lh_zo.h"
+#  elif CGLM_CONFIG_CLIP_CONTROL == CGLM_CLIP_CONTROL_LH_NO
+#    include "clipspace/ortho_lh_no.h"
+#    include "clipspace/persp_lh_no.h"
+#    include "clipspace/view_lh_no.h"
+#  elif CGLM_CONFIG_CLIP_CONTROL == CGLM_CLIP_CONTROL_RH_ZO
+#    include "clipspace/ortho_rh_zo.h"
+#    include "clipspace/persp_rh_zo.h"
+#    include "clipspace/view_rh_zo.h"
+#  elif CGLM_CONFIG_CLIP_CONTROL == CGLM_CLIP_CONTROL_RH_NO
+#    include "clipspace/ortho_rh_no.h"
+#    include "clipspace/persp_rh_no.h"
+#    include "clipspace/view_rh_no.h"
+#  endif
+#else
+#  include "clipspace/ortho_lh_zo.h"
+#  include "clipspace/persp_lh_zo.h"
+#  include "clipspace/ortho_lh_no.h"
+#  include "clipspace/persp_lh_no.h"
+#  include "clipspace/ortho_rh_zo.h"
+#  include "clipspace/persp_rh_zo.h"
+#  include "clipspace/ortho_rh_no.h"
+#  include "clipspace/persp_rh_no.h"
+#  include "clipspace/view_lh_zo.h"
+#  include "clipspace/view_lh_no.h"
+#  include "clipspace/view_rh_zo.h"
+#  include "clipspace/view_rh_no.h"
+#endif
+
 
 /*!
  * if you have axis order like vec3 orderVec = [0, 1, 2] or [0, 2, 1]...
@@ -460,8 +499,8 @@ glm_euler_by_order(vec3 angles, glm_euler_seq ord, mat4 dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in x y z order (roll pitch yaw)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -477,8 +516,8 @@ glm_euler_xyz_quat(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in x z y order (roll yaw pitch)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -494,8 +533,8 @@ glm_euler_xzy_quat(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in y x z order (pitch roll yaw)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -511,8 +550,8 @@ glm_euler_yxz_quat(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in y z x order (pitch yaw roll)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -528,8 +567,8 @@ glm_euler_yzx_quat(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in z x y order (yaw roll pitch)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -545,8 +584,8 @@ glm_euler_zxy_quat(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in z y x order (yaw pitch roll)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
diff --git a/include/cglm/handed/euler_to_quat_lh.h b/include/cglm/handed/euler_to_quat_lh.h
new file mode 100644
index 0000000..def40c9
--- /dev/null
+++ b/include/cglm/handed/euler_to_quat_lh.h
@@ -0,0 +1,167 @@
+/*
+ * Copyright (c), Recep Aslantas.
+ *
+ * MIT License (MIT), http://opensource.org/licenses/MIT
+ * Full license can be found in the LICENSE file
+ */
+
+/*
+ Functions:
+   CGLM_INLINE void glm_euler_xyz_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glm_euler_xzy_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glm_euler_yxz_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glm_euler_yzx_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glm_euler_zxy_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glm_euler_zyx_quat_lh(vec3 angles, versor dest);
+ */
+
+/*
+ Things to note:
+ The only difference between euler to quat rh vs lh is that the zsin part is negative
+ */
+
+#ifndef cglm_euler_to_quat_lh_h
+#define cglm_euler_to_quat_lh_h
+
+#include "../common.h"
+
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in x y z order in left hand (roll pitch yaw)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+void
+glm_euler_xyz_quat_lh(vec3 angles, versor dest) {
+  float xc, yc, zc,
+        xs, ys, zs;
+
+  xs =  sinf(angles[0] * 0.5f); xc = cosf(angles[0] * 0.5f);
+  ys =  sinf(angles[1] * 0.5f); yc = cosf(angles[1] * 0.5f);
+  zs = -sinf(angles[2] * 0.5f); zc = cosf(angles[2] * 0.5f);
+
+  dest[0] = xc * ys * zs + xs * yc * zc;
+  dest[1] = xc * ys * zc - xs * yc * zs;
+  dest[2] = xc * yc * zs + xs * ys * zc;
+  dest[3] = xc * yc * zc - xs * ys * zs;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in x z y order in left hand (roll yaw pitch)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+void
+glm_euler_xzy_quat_lh(vec3 angles, versor dest) {
+  float xc, yc, zc,
+        xs, ys, zs;
+
+  xs =  sinf(angles[0] * 0.5f); xc = cosf(angles[0] * 0.5f);
+  ys =  sinf(angles[1] * 0.5f); yc = cosf(angles[1] * 0.5f);
+  zs = -sinf(angles[2] * 0.5f); zc = cosf(angles[2] * 0.5f);
+
+  dest[0] = -xc * zs * ys + xs * zc * yc;
+  dest[1] =  xc * zc * ys - xs * zs * yc;
+  dest[2] =  xc * zs * yc + xs * zc * ys;
+  dest[3] =  xc * zc * yc + xs * zs * ys;  
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in y x z order in left hand (pitch roll yaw)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+void
+glm_euler_yxz_quat_lh(vec3 angles, versor dest) {
+  float xc, yc, zc,
+        xs, ys, zs;
+
+  xs =  sinf(angles[0] * 0.5f); xc = cosf(angles[0] * 0.5f);
+  ys =  sinf(angles[1] * 0.5f); yc = cosf(angles[1] * 0.5f);
+  zs = -sinf(angles[2] * 0.5f); zc = cosf(angles[2] * 0.5f);
+
+  dest[0] =  yc * xs * zc + ys * xc * zs;
+  dest[1] = -yc * xs * zs + ys * xc * zc;
+  dest[2] =  yc * xc * zs - ys * xs * zc;
+  dest[3] =  yc * xc * zc + ys * xs * zs;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in y z x order in left hand (pitch yaw roll)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+void
+glm_euler_yzx_quat_lh(vec3 angles, versor dest) {
+  float xc, yc, zc,
+        xs, ys, zs;
+
+  xs =  sinf(angles[0] * 0.5f); xc = cosf(angles[0] * 0.5f);
+  ys =  sinf(angles[1] * 0.5f); yc = cosf(angles[1] * 0.5f);
+  zs = -sinf(angles[2] * 0.5f); zc = cosf(angles[2] * 0.5f);
+
+  dest[0] = yc * zc * xs + ys * zs * xc;
+  dest[1] = yc * zs * xs + ys * zc * xc;
+  dest[2] = yc * zs * xc - ys * zc * xs;
+  dest[3] = yc * zc * xc - ys * zs * xs;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in z x y order in left hand (yaw roll pitch)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+void
+glm_euler_zxy_quat_lh(vec3 angles, versor dest) {
+  float xc, yc, zc,
+        xs, ys, zs;
+
+  xs =  sinf(angles[0] * 0.5f); xc = cosf(angles[0] * 0.5f);
+  ys =  sinf(angles[1] * 0.5f); yc = cosf(angles[1] * 0.5f);
+  zs = -sinf(angles[2] * 0.5f); zc = cosf(angles[2] * 0.5f);
+
+  dest[0] = zc * xs * yc - zs * xc * ys;
+  dest[1] = zc * xc * ys + zs * xs * yc;
+  dest[2] = zc * xs * ys + zs * xc * yc;
+  dest[3] = zc * xc * yc - zs * xs * ys;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in z y x order in left hand (yaw pitch roll)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+void
+glm_euler_zyx_quat_lh(vec3 angles, versor dest) {
+  float xc, yc, zc,
+        xs, ys, zs;
+
+  xs =  sinf(angles[0] * 0.5f); xc = cosf(angles[0] * 0.5f);
+  ys =  sinf(angles[1] * 0.5f); yc = cosf(angles[1] * 0.5f);
+  zs = -sinf(angles[2] * 0.5f); zc = cosf(angles[2] * 0.5f);
+
+  dest[0] =  zc * yc * xs - zs * ys * xc;
+  dest[1] =  zc * ys * xc + zs * yc * xs;
+  dest[2] = -zc * ys * xs + zs * yc * xc;
+  dest[3] =  zc * yc * xc + zs * ys * xs;
+}
+
+#endif /*cglm_euler_to_quat_lh_h*/
\ No newline at end of file
diff --git a/include/cglm/handed/euler_to_quat_rh.h b/include/cglm/handed/euler_to_quat_rh.h
index b65108c..aeb6f81 100644
--- a/include/cglm/handed/euler_to_quat_rh.h
+++ b/include/cglm/handed/euler_to_quat_rh.h
@@ -15,6 +15,11 @@
    CGLM_INLINE void glm_euler_zyx_quat_rh(vec3 angles, versor dest);
  */
 
+/*
+ Things to note:
+ The only difference between euler to quat rh vs lh is that the zsin part is negative
+ */
+
 #ifndef cglm_euler_to_quat_rh_h
 #define cglm_euler_to_quat_rh_h
 
@@ -24,8 +29,8 @@
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in x y z order in right hand (roll pitch yaw)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -48,8 +53,8 @@ glm_euler_xyz_quat_rh(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in x z y order in right hand (roll yaw pitch)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -72,8 +77,8 @@ glm_euler_xzy_quat_rh(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in y x z order in right hand (pitch roll yaw)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -95,8 +100,8 @@ glm_euler_yxz_quat_rh(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in y z x order in right hand (pitch yaw roll)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -119,8 +124,8 @@ glm_euler_yzx_quat_rh(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in z x y order in right hand (yaw roll pitch)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
@@ -142,8 +147,8 @@ glm_euler_zxy_quat_rh(vec3 angles, versor dest) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in z y x order in right hand (yaw pitch roll)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 void
diff --git a/include/cglm/struct/euler.h b/include/cglm/struct/euler.h
index 7b75946..3395745 100644
--- a/include/cglm/struct/euler.h
+++ b/include/cglm/struct/euler.h
@@ -159,8 +159,8 @@ glms_euler_by_order(vec3s angles, glm_euler_seq ord) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in x y z order (roll pitch yaw)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 versors
@@ -174,8 +174,8 @@ glms_euler_xyz_quat(vec3s angles) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in x z y order (roll yaw pitch)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 versors
@@ -189,8 +189,8 @@ glms_euler_xzy_quat(vec3s angles) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in y x z order (pitch roll yaw)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 versors
@@ -204,8 +204,8 @@ glms_euler_yxz_quat(vec3s angles) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in y z x order (pitch yaw roll)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 versors
@@ -219,8 +219,8 @@ glms_euler_yzx_quat(vec3s angles) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in z x y order (yaw roll pitch)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 versors
@@ -234,8 +234,8 @@ glms_euler_zxy_quat(vec3s angles) {
  * @brief creates NEW quaternion using rotation angles and does
  *        rotations in z y x order (yaw pitch roll)
  * 
- * @param[out]  q     quaternion
- * @param[in]   angle angles x y z (radians)
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
  */
 CGLM_INLINE
 versors
diff --git a/include/cglm/struct/handed/euler_to_quat_lh.h b/include/cglm/struct/handed/euler_to_quat_lh.h
new file mode 100644
index 0000000..3964e51
--- /dev/null
+++ b/include/cglm/struct/handed/euler_to_quat_lh.h
@@ -0,0 +1,115 @@
+/*
+ * Copyright (c), Recep Aslantas.
+ *
+ * MIT License (MIT), http://opensource.org/licenses/MIT
+ * Full license can be found in the LICENSE file
+ */
+
+/*
+ Functions:
+   CGLM_INLINE void glms_euler_xyz_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_xzy_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_yxz_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_yzx_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_zxy_quat_lh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_zyx_quat_lh(vec3 angles, versor dest);
+ */
+
+#ifndef cglms_euler_to_quat_lh_h
+#define cglms_euler_to_quat_lh_h
+
+#include "../common.h"
+
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in x y z order in left hand (roll pitch yaw)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_xyz_quat_lh(vec3s angles) {
+  versors dest;
+  glm_euler_xyz_quat_lh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in x z y order in left hand (roll yaw pitch)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_xzy_quat_lh(vec3s angles) {
+  versors dest;
+  glm_euler_xzy_quat_lh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in y x z order in left hand (pitch roll yaw)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_yxz_quat_lh(vec3s angles) {
+  versors dest;
+  glm_euler_yxz_quat_lh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in y z x order in left hand (pitch yaw roll)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_yzx_quat_lh(vec3s angles) {
+  versors dest;
+  glm_euler_yzx_quat_lh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in z x y order in left hand (yaw roll pitch)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_zxy_quat_lh(vec3s angles) {
+  versors dest;
+  glm_euler_zxy_quat_lh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in z y x order in left hand (yaw pitch roll)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_zyx_quat_lh(vec3s angles) {
+  versors dest;
+  glm_euler_zyx_quat_lh(angles.raw, dest.raw);
+  return dest;
+}
+
+
+#endif /* cglms_euler_to_quat_lh_h */
diff --git a/include/cglm/struct/handed/euler_to_quat_rh.h b/include/cglm/struct/handed/euler_to_quat_rh.h
new file mode 100644
index 0000000..6c7f400
--- /dev/null
+++ b/include/cglm/struct/handed/euler_to_quat_rh.h
@@ -0,0 +1,115 @@
+/*
+ * Copyright (c), Recep Aslantas.
+ *
+ * MIT License (MIT), http://opensource.org/licenses/MIT
+ * Full license can be found in the LICENSE file
+ */
+
+/*
+ Functions:
+   CGLM_INLINE void glms_euler_xyz_quat_rh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_xzy_quat_rh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_yxz_quat_rh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_yzx_quat_rh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_zxy_quat_rh(vec3 angles, versor dest);
+   CGLM_INLINE void glms_euler_zyx_quat_rh(vec3 angles, versor dest);
+ */
+
+#ifndef cglms_euler_to_quat_rh_h
+#define cglms_euler_to_quat_rh_h
+
+#include "../common.h"
+
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in x y z order in right hand (roll pitch yaw)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_xyz_quat_rh(vec3s angles) {
+  versors dest;
+  glm_euler_xyz_quat_rh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in x z y order in right hand (roll yaw pitch)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_xzy_quat_rh(vec3s angles) {
+  versors dest;
+  glm_euler_xzy_quat_rh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in y x z order in right hand (pitch roll yaw)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_yxz_quat_rh(vec3s angles) {
+  versors dest;
+  glm_euler_yxz_quat_rh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in y z x order in right hand (pitch yaw roll)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_yzx_quat_rh(vec3s angles) {
+  versors dest;
+  glm_euler_yzx_quat_rh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in z x y order in right hand (yaw roll pitch)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_zxy_quat_rh(vec3s angles) {
+  versors dest;
+  glm_euler_zxy_quat_rh(angles.raw, dest.raw);
+  return dest;
+}
+
+/*!
+ * @brief creates NEW quaternion using rotation angles and does
+ *        rotations in z y x order in right hand (yaw pitch roll)
+ * 
+ * @param[in]   angles angles x y z (radians)
+ * @param[out]  dest   quaternion
+ */
+CGLM_INLINE
+versors
+glms_euler_zyx_quat_rh(vec3s angles) {
+  versors dest;
+  glm_euler_zyx_quat_rh(angles.raw, dest.raw);
+  return dest;
+}
+
+
+#endif /* cglms_euler_to_quat_rh_h */
diff --git a/test/src/test_euler_to_quat_lh.h b/test/src/test_euler_to_quat_lh.h
new file mode 100644
index 0000000..faec48e
--- /dev/null
+++ b/test/src/test_euler_to_quat_lh.h
@@ -0,0 +1,495 @@
+/*
+ * Copyright (c), Recep Aslantas.
+ *
+ * MIT License (MIT), http://opensource.org/licenses/MIT
+ * Full license can be found in the LICENSE file
+ */
+
+#include "test_common.h"
+#include "../../include/cglm/handed/euler_to_quat_lh.h"
+
+TEST_IMPL(GLM_PREFIX, euler_xyz_quat_lh) {
+  vec3 axis_x = {1.0f, 0.0f, 0.0f};
+  vec3 axis_y = {0.0f, 1.0f, 0.0f};
+  vec3 axis_z = {0.0f, 0.0f,-1.0f};
+
+  /* random angles for testing */
+  vec3 angles;
+
+  /* quaternion representations for rotations */
+  versor rot_x, rot_y, rot_z;
+
+  versor expected;
+  versor result;
+  versor tmp;
+
+  /* 100 randomized tests */
+  for (int i = 0; i < 100; i++) {
+    test_rand_vec3(angles);
+
+    /* create the rotation quaternions using the angles and axises */
+    glm_quatv(rot_x, angles[0], axis_x);
+    glm_quatv(rot_y, angles[1], axis_y);
+    glm_quatv(rot_z, angles[2], axis_z);
+
+    /* apply the rotations to a unit quaternion in xyz order */
+    glm_quat_identity(expected);
+
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_x, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_y, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_z, expected);
+
+    glm_euler_xyz_quat_lh(angles, result);
+
+    /* verify if the magnitude of the quaternion stays 1 */
+    ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+    /* verify that it acts the same as rotating by 3 axis quaternions */
+    ASSERTIFY(test_assert_quat_eq(result, expected))
+  }
+  
+
+  /* Start gimbal lock tests */
+  for (float x = -90.0f; x <= 90.0f; x += 90.0f) {
+    for (float y = -90.0f; y <= 90.0f; y += 90.0f) {
+      for (float z = -90.0f; z <= 90.0f; z += 90.0f) {
+        angles[0] = x;
+        angles[1] = y;
+        angles[2] = z;
+        
+        /* create the rotation quaternions using the angles and axises */
+        glm_quatv(rot_x, angles[0], axis_x);
+        glm_quatv(rot_y, angles[1], axis_y);
+        glm_quatv(rot_z, angles[2], axis_z);
+
+        /* apply the rotations to a unit quaternion in xyz order */
+        glm_quat_identity(expected);
+        
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_x, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_y, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_z, expected);
+    
+        /* use my function to get the quaternion */
+        glm_euler_xyz_quat_lh(angles, result);
+
+        /* verify if the magnitude of the quaternion stays 1 */
+        ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+        /* verify that it acts the same as rotating by 3 axis quaternions */
+        ASSERTIFY(test_assert_quat_eq(result, expected))
+      }
+    }
+  }
+  TEST_SUCCESS
+}
+
+TEST_IMPL(GLM_PREFIX, euler_xzy_quat_lh) {
+  vec3 axis_x = {1.0f, 0.0f, 0.0f};
+  vec3 axis_y = {0.0f, 1.0f, 0.0f};
+  vec3 axis_z = {0.0f, 0.0f,-1.0f};
+
+  /* random angles for testing */
+  vec3 angles;
+
+  /* quaternion representations for rotations */
+  versor rot_x, rot_y, rot_z;
+
+  versor expected;
+  versor result;
+  versor tmp;
+
+  /* 100 randomized tests */
+  for (int i = 0; i < 100; i++) {
+    test_rand_vec3(angles);
+
+    /* create the rotation quaternions using the angles and axises */
+    glm_quatv(rot_x, angles[0], axis_x);
+    glm_quatv(rot_y, angles[1], axis_y);
+    glm_quatv(rot_z, angles[2], axis_z);
+
+    /* apply the rotations to a unit quaternion in xzy order */
+    glm_quat_identity(expected);
+    
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_x, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_z, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_y, expected);
+
+    glm_euler_xzy_quat_lh(angles, result);
+
+    /* verify if the magnitude of the quaternion stays 1 */
+    ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+    /* verify that it acts the same as rotating by 3 axis quaternions */
+    ASSERTIFY(test_assert_quat_eq(result, expected))
+  }
+  
+
+  /* Start gimbal lock tests */
+  for (float x = -90.0f; x <= 90.0f; x += 90.0f) {
+    for (float y = -90.0f; y <= 90.0f; y += 90.0f) {
+      for (float z = -90.0f; z <= 90.0f; z += 90.0f) {
+        angles[0] = x;
+        angles[1] = y;
+        angles[2] = z;
+        
+        /* create the rotation quaternions using the angles and axises */
+        glm_quatv(rot_x, angles[0], axis_x);
+        glm_quatv(rot_y, angles[1], axis_y);
+        glm_quatv(rot_z, angles[2], axis_z);
+
+        /* apply the rotations to a unit quaternion in xzy order */
+        glm_quat_identity(expected);
+        
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_x, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_z, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_y, expected);
+
+        /* use my function to get the quaternion */
+        glm_euler_xzy_quat_lh(angles, result);
+
+        /* verify if the magnitude of the quaternion stays 1 */
+        ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+        /* verify that it acts the same as rotating by 3 axis quaternions */
+        ASSERTIFY(test_assert_quat_eq(result, expected))
+      }
+    }
+  }
+  TEST_SUCCESS
+}
+
+TEST_IMPL(GLM_PREFIX, euler_yxz_quat_lh) {
+  vec3 axis_x = {1.0f, 0.0f, 0.0f};
+  vec3 axis_y = {0.0f, 1.0f, 0.0f};
+  vec3 axis_z = {0.0f, 0.0f,-1.0f};
+
+  /* random angles for testing */
+  vec3 angles;
+
+  /* quaternion representations for rotations */
+  versor rot_x, rot_y, rot_z;
+
+  versor expected;
+  versor result;
+  versor tmp;
+
+  /* 100 randomized tests */
+  for (int i = 0; i < 100; i++) {
+    test_rand_vec3(angles);
+
+    /* create the rotation quaternions using the angles and axises */
+    glm_quatv(rot_x, angles[0], axis_x);
+    glm_quatv(rot_y, angles[1], axis_y);
+    glm_quatv(rot_z, angles[2], axis_z);
+
+    /* apply the rotations to a unit quaternion in yxz order */
+    glm_quat_identity(expected);
+    
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_y, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_x, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_z, expected);
+
+    glm_euler_yxz_quat_lh(angles, result);
+
+    /* verify if the magnitude of the quaternion stays 1 */
+    ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+    /* verify that it acts the same as rotating by 3 axis quaternions */
+    ASSERTIFY(test_assert_quat_eq(result, expected))
+  }
+  
+
+  /* Start gimbal lock tests */
+  for (float x = -90.0f; x <= 90.0f; x += 90.0f) {
+    for (float y = -90.0f; y <= 90.0f; y += 90.0f) {
+      for (float z = -90.0f; z <= 90.0f; z += 90.0f) {
+        angles[0] = x;
+        angles[1] = y;
+        angles[2] = z;
+        
+        /* create the rotation quaternions using the angles and axises */
+        glm_quatv(rot_x, angles[0], axis_x);
+        glm_quatv(rot_y, angles[1], axis_y);
+        glm_quatv(rot_z, angles[2], axis_z);
+
+        /* apply the rotations to a unit quaternion in yxz order */
+        glm_quat_identity(expected);
+        
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_y, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_x, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_z, expected);
+
+        /* use my function to get the quaternion */
+        glm_euler_yxz_quat_lh(angles, result);
+
+        /* verify if the magnitude of the quaternion stays 1 */
+        ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+        ASSERTIFY(test_assert_quat_eq(result, expected))
+      }
+    }
+  }
+  TEST_SUCCESS
+}
+
+TEST_IMPL(GLM_PREFIX, euler_yzx_quat_lh) {
+  vec3 axis_x = {1.0f, 0.0f, 0.0f};
+  vec3 axis_y = {0.0f, 1.0f, 0.0f};
+  vec3 axis_z = {0.0f, 0.0f,-1.0f};
+
+  /* random angles for testing */
+  vec3 angles;
+
+  /* quaternion representations for rotations */
+  versor rot_x, rot_y, rot_z;
+
+  versor expected;
+  versor result;
+  versor tmp;
+
+  /* 100 randomized tests */
+  for (int i = 0; i < 100; i++) {
+    test_rand_vec3(angles);
+
+    /* create the rotation quaternions using the angles and axises */
+    glm_quatv(rot_x, angles[0], axis_x);
+    glm_quatv(rot_y, angles[1], axis_y);
+    glm_quatv(rot_z, angles[2], axis_z);
+
+    /* apply the rotations to a unit quaternion in yzx order */
+    glm_quat_identity(expected);
+    
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_y, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_z, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_x, expected);
+
+    glm_euler_yzx_quat_lh(angles, result);
+
+    /* verify if the magnitude of the quaternion stays 1 */
+    ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+    /* verify that it acts the same as rotating by 3 axis quaternions */
+    ASSERTIFY(test_assert_quat_eq(result, expected))
+  }
+  
+
+  /* Start gimbal lock tests */
+  for (float x = -90.0f; x <= 90.0f; x += 90.0f) {
+    for (float y = -90.0f; y <= 90.0f; y += 90.0f) {
+      for (float z = -90.0f; z <= 90.0f; z += 90.0f) {
+        angles[0] = x;
+        angles[1] = y;
+        angles[2] = z;
+        
+        /* create the rotation quaternions using the angles and axises */
+        glm_quatv(rot_x, angles[0], axis_x);
+        glm_quatv(rot_y, angles[1], axis_y);
+        glm_quatv(rot_z, angles[2], axis_z);
+
+        /* apply the rotations to a unit quaternion in yzx order */
+        glm_quat_identity(expected);
+        
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_y, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_z, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_x, expected);
+
+        /* use my function to get the quaternion */
+        glm_euler_yzx_quat_lh(angles, result);
+
+        /* verify if the magnitude of the quaternion stays 1 */
+        ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+        ASSERTIFY(test_assert_quat_eq(result, expected))
+      }
+    }
+  }
+  TEST_SUCCESS
+}
+
+TEST_IMPL(GLM_PREFIX, euler_zxy_quat_lh) {
+  vec3 axis_x = {1.0f, 0.0f, 0.0f};
+  vec3 axis_y = {0.0f, 1.0f, 0.0f};
+  vec3 axis_z = {0.0f, 0.0f,-1.0f};
+
+  /* random angles for testing */
+  vec3 angles;
+
+  /* quaternion representations for rotations */
+  versor rot_x, rot_y, rot_z;
+
+  versor expected;
+  versor result;
+  versor tmp;
+
+  /* 100 randomized tests */
+  for (int i = 0; i < 100; i++) {
+    test_rand_vec3(angles);
+
+    /* create the rotation quaternions using the angles and axises */
+    glm_quatv(rot_x, angles[0], axis_x);
+    glm_quatv(rot_y, angles[1], axis_y);
+    glm_quatv(rot_z, angles[2], axis_z);
+
+    /* apply the rotations to a unit quaternion in zxy order */
+    glm_quat_identity(expected);
+
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_z, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_x, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_y, expected);
+
+    glm_euler_zxy_quat_lh(angles, result);
+
+    /* verify if the magnitude of the quaternion stays 1 */
+    ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+    /* verify that it acts the same as rotating by 3 axis quaternions */
+    ASSERTIFY(test_assert_quat_eq(result, expected))
+  }
+  
+
+  /* Start gimbal lock tests */
+  for (float x = -90.0f; x <= 90.0f; x += 90.0f) {
+    for (float y = -90.0f; y <= 90.0f; y += 90.0f) {
+      for (float z = -90.0f; z <= 90.0f; z += 90.0f) {
+        angles[0] = x;
+        angles[1] = y;
+        angles[2] = z;
+        
+        /* create the rotation quaternions using the angles and axises */
+        glm_quatv(rot_x, angles[0], axis_x);
+        glm_quatv(rot_y, angles[1], axis_y);
+        glm_quatv(rot_z, angles[2], axis_z);
+
+        /* apply the rotations to a unit quaternion in zxy order */
+        glm_quat_identity(expected);
+
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_z, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_x, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_y, expected);
+
+        /* use my function to get the quaternion */
+        glm_euler_zxy_quat_lh(angles, result);
+
+        /* verify if the magnitude of the quaternion stays 1 */
+        ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+        /* verify that it acts the same as rotating by 3 axis quaternions */
+        ASSERTIFY(test_assert_quat_eq(result, expected))
+      }
+    }
+  }
+  TEST_SUCCESS
+}
+
+TEST_IMPL(GLM_PREFIX, euler_zyx_quat_lh) {
+  vec3 axis_x = {1.0f, 0.0f, 0.0f};
+  vec3 axis_y = {0.0f, 1.0f, 0.0f};
+  vec3 axis_z = {0.0f, 0.0f,-1.0f};
+
+  /* random angles for testing */
+  vec3 angles;
+
+  /* quaternion representations for rotations */
+  versor rot_x, rot_y, rot_z;
+
+  versor expected;
+  versor result;
+  versor tmp;
+
+  /* 100 randomized tests */
+  for (int i = 0; i < 100; i++) {
+    test_rand_vec3(angles);
+
+    /* create the rotation quaternions using the angles and axises */
+    glm_quatv(rot_x, angles[0], axis_x);
+    glm_quatv(rot_y, angles[1], axis_y);
+    glm_quatv(rot_z, angles[2], axis_z);
+
+    /* apply the rotations to a unit quaternion in zyx order */
+    glm_quat_identity(expected);
+
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_z, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_y, expected);
+    glm_quat_copy(expected, tmp);
+    glm_quat_mul(tmp, rot_x, expected);
+
+    glm_euler_zyx_quat_lh(angles, result);
+
+    /* verify if the magnitude of the quaternion stays 1 */
+    ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+    /* verify that it acts the same as rotating by 3 axis quaternions */
+    ASSERTIFY(test_assert_quat_eq(result, expected))
+  }
+  
+
+  /* Start gimbal lock tests */
+  for (float x = -90.0f; x <= 90.0f; x += 90.0f) {
+    for (float y = -90.0f; y <= 90.0f; y += 90.0f) {
+      for (float z = -90.0f; z <= 90.0f; z += 90.0f) {
+        angles[0] = x;
+        angles[1] = y;
+        angles[2] = z;
+        
+        /* create the rotation quaternions using the angles and axises */
+        glm_quatv(rot_x, angles[0], axis_x);
+        glm_quatv(rot_y, angles[1], axis_y);
+        glm_quatv(rot_z, angles[2], axis_z);
+
+        /* apply the rotations to a unit quaternion in xyz order */
+        glm_quat_identity(expected);
+        
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_z, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_y, expected);
+        glm_quat_copy(expected, tmp);
+        glm_quat_mul(tmp, rot_x, expected);
+
+        /* use my function to get the quaternion */
+        glm_euler_zyx_quat_lh(angles, result);
+
+        /* verify if the magnitude of the quaternion stays 1 */
+        ASSERT(test_eq(glm_quat_norm(result), 1.0f))
+
+        /* verify that it acts the same as rotating by 3 axis quaternions */
+        ASSERTIFY(test_assert_quat_eq(result, expected))
+      }
+    }
+  }
+  TEST_SUCCESS
+}
+
+
diff --git a/test/src/tests.c b/test/src/tests.c
index 274f7e0..4d93294 100644
--- a/test/src/tests.c
+++ b/test/src/tests.c
@@ -40,6 +40,7 @@
 #include "test_cam_rh_no.h"
 #include "test_cam_rh_zo.h"
 #include "test_euler_to_quat_rh.h"
+#include "test_euler_to_quat_lh.h"
 
 #undef GLM
 #undef GLM_PREFIX
@@ -78,6 +79,7 @@
 #include "test_cam_rh_no.h"
 #include "test_cam_rh_zo.h"
 #include "test_euler_to_quat_rh.h"
+#include "test_euler_to_quat_lh.h"
 
 #undef GLM
 #undef GLM_PREFIX
diff --git a/test/tests.h b/test/tests.h
index a27295d..432f16d 100644
--- a/test/tests.h
+++ b/test/tests.h
@@ -363,9 +363,31 @@ TEST_DECLARE(clamp)
 TEST_DECLARE(glm_euler_xyz_quat_rh) 
 TEST_DECLARE(glm_euler_xzy_quat_rh) 
 TEST_DECLARE(glm_euler_yxz_quat_rh)
-TEST_DECLARE(glm_euler_yzx_quat_rh)  
+TEST_DECLARE(glm_euler_yzx_quat_rh) 
 TEST_DECLARE(glm_euler_zxy_quat_rh)
 TEST_DECLARE(glm_euler_zyx_quat_rh)
+
+TEST_DECLARE(glm_euler_xyz_quat_lh) 
+TEST_DECLARE(glm_euler_xzy_quat_lh) 
+TEST_DECLARE(glm_euler_yxz_quat_lh)
+TEST_DECLARE(glm_euler_yzx_quat_lh) 
+TEST_DECLARE(glm_euler_zxy_quat_lh)
+TEST_DECLARE(glm_euler_zyx_quat_lh)
+
+TEST_DECLARE(glmc_euler_xyz_quat_rh) 
+TEST_DECLARE(glmc_euler_xzy_quat_rh) 
+TEST_DECLARE(glmc_euler_yxz_quat_rh)
+TEST_DECLARE(glmc_euler_yzx_quat_rh)  
+TEST_DECLARE(glmc_euler_zxy_quat_rh)
+TEST_DECLARE(glmc_euler_zyx_quat_rh)
+
+TEST_DECLARE(glmc_euler_xyz_quat_lh) 
+TEST_DECLARE(glmc_euler_xzy_quat_lh) 
+TEST_DECLARE(glmc_euler_yxz_quat_lh)
+TEST_DECLARE(glmc_euler_yzx_quat_lh)  
+TEST_DECLARE(glmc_euler_zxy_quat_lh)
+TEST_DECLARE(glmc_euler_zyx_quat_lh)
+
 TEST_DECLARE(euler)
 
 /* ray */
@@ -1481,6 +1503,28 @@ TEST_LIST {
   TEST_ENTRY(glm_euler_yzx_quat_rh)  
   TEST_ENTRY(glm_euler_zxy_quat_rh)
   TEST_ENTRY(glm_euler_zyx_quat_rh)
+
+  TEST_ENTRY(glm_euler_xyz_quat_lh)
+  TEST_ENTRY(glm_euler_xzy_quat_lh)
+  TEST_ENTRY(glm_euler_yxz_quat_lh)
+  TEST_ENTRY(glm_euler_yzx_quat_lh)
+  TEST_ENTRY(glm_euler_zxy_quat_lh)
+  TEST_ENTRY(glm_euler_zyx_quat_lh)
+
+  TEST_ENTRY(glmc_euler_xyz_quat_rh) 
+  TEST_ENTRY(glmc_euler_xzy_quat_rh) 
+  TEST_ENTRY(glmc_euler_yxz_quat_rh)
+  TEST_ENTRY(glmc_euler_yzx_quat_rh)  
+  TEST_ENTRY(glmc_euler_zxy_quat_rh)
+  TEST_ENTRY(glmc_euler_zyx_quat_rh)
+
+  TEST_ENTRY(glmc_euler_xyz_quat_lh)
+  TEST_ENTRY(glmc_euler_xzy_quat_lh)
+  TEST_ENTRY(glmc_euler_yxz_quat_lh)
+  TEST_ENTRY(glmc_euler_yzx_quat_lh)
+  TEST_ENTRY(glmc_euler_zxy_quat_lh)
+  TEST_ENTRY(glmc_euler_zyx_quat_lh)
+
   TEST_ENTRY(euler)
   
   /* ray */