mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-06-11 09:32:57 +08:00
Rebase of changes to sensor_hil_fixedwing branch.
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+53
-24
@@ -52,6 +52,23 @@ Dcm::Dcm() :
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{
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}
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Dcm::Dcm(float c00, float c01, float c02,
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float c10, float c11, float c12,
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float c20, float c21, float c22) :
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Matrix(3, 3)
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{
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Dcm &dcm = *this;
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dcm(0,0) = c00;
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dcm(0,1) = c01;
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dcm(0,2) = c02;
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dcm(1,0) = c10;
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dcm(1,1) = c11;
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dcm(1,2) = c12;
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dcm(2,0) = c20;
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dcm(2,1) = c21;
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dcm(2,2) = c22;
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}
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Dcm::Dcm(const float *data) :
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Matrix(3, 3, data)
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{
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@@ -61,22 +78,22 @@ Dcm::Dcm(const Quaternion &q) :
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Matrix(3, 3)
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{
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Dcm &dcm = *this;
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float a = q.getA();
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float b = q.getB();
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float c = q.getC();
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float d = q.getD();
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float aSq = a * a;
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float bSq = b * b;
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float cSq = c * c;
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float dSq = d * d;
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double a = q.getA();
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double b = q.getB();
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double c = q.getC();
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double d = q.getD();
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double aSq = a * a;
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double bSq = b * b;
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double cSq = c * c;
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double dSq = d * d;
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dcm(0, 0) = aSq + bSq - cSq - dSq;
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dcm(0, 1) = 2 * (b * c - a * d);
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dcm(0, 2) = 2 * (a * c + b * d);
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dcm(1, 0) = 2 * (b * c + a * d);
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dcm(0, 1) = 2.0 * (b * c - a * d);
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dcm(0, 2) = 2.0 * (a * c + b * d);
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dcm(1, 0) = 2.0 * (b * c + a * d);
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dcm(1, 1) = aSq - bSq + cSq - dSq;
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dcm(1, 2) = 2 * (c * d - a * b);
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dcm(2, 0) = 2 * (b * d - a * c);
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dcm(2, 1) = 2 * (a * b + c * d);
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dcm(1, 2) = 2.0 * (c * d - a * b);
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dcm(2, 0) = 2.0 * (b * d - a * c);
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dcm(2, 1) = 2.0 * (a * b + c * d);
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dcm(2, 2) = aSq - bSq - cSq + dSq;
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}
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@@ -84,12 +101,12 @@ Dcm::Dcm(const EulerAngles &euler) :
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Matrix(3, 3)
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{
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Dcm &dcm = *this;
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float cosPhi = cosf(euler.getPhi());
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float sinPhi = sinf(euler.getPhi());
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float cosThe = cosf(euler.getTheta());
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float sinThe = sinf(euler.getTheta());
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float cosPsi = cosf(euler.getPsi());
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float sinPsi = sinf(euler.getPsi());
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double cosPhi = cos(euler.getPhi());
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double sinPhi = sin(euler.getPhi());
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double cosThe = cos(euler.getTheta());
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double sinThe = sin(euler.getTheta());
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double cosPsi = cos(euler.getPsi());
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double sinPsi = sin(euler.getPsi());
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dcm(0, 0) = cosThe * cosPsi;
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dcm(0, 1) = -cosPhi * sinPsi + sinPhi * sinThe * cosPsi;
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@@ -116,11 +133,23 @@ Dcm::~Dcm()
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int __EXPORT dcmTest()
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{
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printf("Test DCM\t\t: ");
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// default ctor
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ASSERT(matrixEqual(Dcm(),
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Matrix::identity(3)));
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// quaternion ctor
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ASSERT(matrixEqual(
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Dcm(Quaternion(0.983347, 0.034271, 0.106021, 0.143572)),
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Dcm( 0.9362934, -0.2750958, 0.2183507,
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0.2896295, 0.9564251, -0.0369570,
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-0.1986693, 0.0978434, 0.9751703)));
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// euler angle ctor
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ASSERT(matrixEqual(
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Dcm(EulerAngles(0.1, 0.2, 0.3)),
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Dcm( 0.9362934, -0.2750958, 0.2183507,
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0.2896295, 0.9564251, -0.0369570,
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-0.1986693, 0.0978434, 0.9751703)));
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// rotations
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Vector3 vB(1, 2, 3);
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ASSERT(matrixEqual(Dcm(Quaternion(1, 0, 0, 0)),
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Matrix::identity(3)));
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ASSERT(matrixEqual(Dcm(EulerAngles(0, 0, 0)),
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Matrix::identity(3)));
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ASSERT(vectorEqual(Vector3(-2, 1, 3),
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Dcm(EulerAngles(0, 0, M_PI_2_F))*vB));
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ASSERT(vectorEqual(Vector3(3, 2, -1),
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