Skip to content
New issue

Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.

By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.

Already on GitHub? Sign in to your account

adding method to convert heading pitch roll in quaternion defined in … #4048

Merged
merged 3 commits into from
Jun 28, 2016
Merged
Show file tree
Hide file tree
Changes from all commits
Commits
File filter

Filter by extension

Filter by extension

Conversations
Failed to load comments.
Loading
Jump to
Jump to file
Failed to load files.
Loading
Diff view
Diff view
2 changes: 1 addition & 1 deletion CHANGES.md
Original file line number Diff line number Diff line change
Expand Up @@ -20,9 +20,9 @@ Change Log
* Added the hot air balloon sample model.
* Fixed handling of sampled Rectangle coordinates in CZML. [#4033](https://github.com/AnalyticalGraphicsInc/cesium/pull/4033)
* Fix "Cannot read property 'x' of undefined" error when calling SceneTransforms.wgs84ToWindowCoordinates in certain cases. [#4022](https://github.com/AnalyticalGraphicsInc/cesium/pull/4022)
* Added transform functions to generate 4X4 matrix or quaternion from heading, pitch, roll of an aircraft (use of North East Down local reference)
* Exposed a parametric ray-triangle intersection test to the API as `IntersectionTests.rayTriangleParametric`.


### 1.22.2 - 2016-06-14
* This is an npm only release to fix the improperly published 1.22.1. There were no code changes.

Expand Down
59 changes: 59 additions & 0 deletions Source/Core/Transforms.js
Original file line number Diff line number Diff line change
Expand Up @@ -381,6 +381,36 @@ define([
return Matrix4.multiply(result, hprMatrix, result);
};

/**
* Computes a 4x4 transformation matrix from a reference frame with axes computed from the heading-pitch-roll angles
* centered at the provided origin to the provided ellipsoid's fixed reference frame. Heading is the rotation from the local north
* direction where a positive angle is increasing eastward. Pitch is the rotation from the local east-north plane. Positive pitch angles
* are above the plane. Negative pitch angles are below the plane. Roll is the first rotation applied about the local east axis.
*
* @param {Cartesian3} origin The center point of the local reference frame.
* @param {Number} heading The heading angle in radians.
* @param {Number} pitch The pitch angle in radians.
* @param {Number} roll The roll angle in radians.
* @param {Ellipsoid} [ellipsoid=Ellipsoid.WGS84] The ellipsoid whose fixed frame is used in the transformation.
* @param {Matrix4} [result] The object onto which to store the result.
* @returns {Matrix4} The modified result parameter or a new Matrix4 instance if none was provided.
*
* @example
* // Get the transform from local heading-pitch-roll at cartographic (0.0, 0.0) to Earth's fixed frame.
* var center = Cesium.Cartesian3.fromDegrees(0.0, 0.0);
* var heading = -Cesium.Math.PI_OVER_TWO;
* var pitch = Cesium.Math.PI_OVER_FOUR;
* var roll = 0.0;
* var transform = Cesium.Transforms.aircraftHeadingPitchRollToFixedFrame(center, heading, pitch, roll);
*/
Transforms.aircraftHeadingPitchRollToFixedFrame = function(origin, heading, pitch, roll, ellipsoid, result) {
// checks for required parameters happen in the called functions
Copy link
Contributor

Choose a reason for hiding this comment

The reason will be displayed to describe this comment to others. Learn more.

Can you still add unit tests for these with toThrowDeveloperError?

var hprQuaternion = Quaternion.fromHeadingPitchRoll(heading, pitch, roll, scratchHPRQuaternion);
var hprMatrix = Matrix4.fromTranslationQuaternionRotationScale(Cartesian3.ZERO, hprQuaternion, scratchScale, scratchHPRMatrix4);
result = Transforms.northEastDownToFixedFrame(origin, ellipsoid, result);
return Matrix4.multiply(result, hprMatrix, result);
};

var scratchENUMatrix4 = new Matrix4();
var scratchHPRMatrix3 = new Matrix3();

Expand Down Expand Up @@ -413,6 +443,35 @@ define([
return Quaternion.fromRotationMatrix(rotation, result);
};

/**
* Computes a quaternion from a reference frame with axes computed from the heading-pitch-roll angles
* centered at the provided origin. Heading is the rotation from the local north
* direction where a positive angle is increasing eastward. Pitch is the rotation from the local east-north plane. Positive pitch angles
* are above the plane. Negative pitch angles are below the plane. Roll is the first rotation applied about the local east axis.
*
* @param {Cartesian3} origin The center point of the local reference frame.
* @param {Number} heading The heading angle in radians.
* @param {Number} pitch The pitch angle in radians.
* @param {Number} roll The roll angle in radians.
* @param {Ellipsoid} [ellipsoid=Ellipsoid.WGS84] The ellipsoid whose fixed frame is used in the transformation.
* @param {Quaternion} [result] The object onto which to store the result.
* @returns {Quaternion} The modified result parameter or a new Quaternion instance if none was provided.
*
* @example
* // Get the quaternion from local heading-pitch-roll at cartographic (0.0, 0.0) to Earth's fixed frame.
* var center = Cesium.Cartesian3.fromDegrees(0.0, 0.0);
* var heading = -Cesium.Math.PI_OVER_TWO;
* var pitch = Cesium.Math.PI_OVER_FOUR;
* var roll = 0.0;
* var quaternion = Cesium.Transforms.aircraftHeadingPitchRollQuaternion(center, heading, pitch, roll);
*/
Transforms.aircraftHeadingPitchRollQuaternion = function(origin, heading, pitch, roll, ellipsoid, result) {
// checks for required parameters happen in the called functions
Copy link
Contributor

Choose a reason for hiding this comment

The reason will be displayed to describe this comment to others. Learn more.

Same comment.

var transform = Transforms.aircraftHeadingPitchRollToFixedFrame(origin, heading, pitch, roll, ellipsoid, scratchENUMatrix4);
var rotation = Matrix4.getRotation(transform, scratchHPRMatrix3);
return Quaternion.fromRotationMatrix(rotation, result);
};


var gmstConstant0 = 6 * 3600 + 41 * 60 + 50.54841;
var gmstConstant1 = 8640184.812866;
Expand Down
134 changes: 134 additions & 0 deletions Specs/Core/TransformsSpec.js
Original file line number Diff line number Diff line change
Expand Up @@ -243,6 +243,62 @@ defineSuite([
expect(actualTranslation).toEqual(origin);
});

it('aircraftHeadingPitchRollToFixedFrame works without a result parameter', function() {
var origin = new Cartesian3(1.0, 0.0, 0.0);
var heading = CesiumMath.toRadians(20.0);
var pitch = CesiumMath.toRadians(30.0);
var roll = CesiumMath.toRadians(40.0);

var expectedRotation = Matrix3.fromQuaternion(Quaternion.fromHeadingPitchRoll(heading, pitch, roll));
var expectedX = Matrix3.getColumn(expectedRotation, 0, new Cartesian3());
var expectedY = Matrix3.getColumn(expectedRotation, 1, new Cartesian3());
var expectedZ = Matrix3.getColumn(expectedRotation, 2, new Cartesian3());

Cartesian3.fromElements(-expectedX.z, expectedX.y, expectedX.x, expectedX);
Cartesian3.fromElements(-expectedY.z, expectedY.y, expectedY.x, expectedY);
Cartesian3.fromElements(-expectedZ.z, expectedZ.y, expectedZ.x, expectedZ);

var returnedResult = Transforms.aircraftHeadingPitchRollToFixedFrame(origin, heading, pitch, roll, Ellipsoid.UNIT_SPHERE);
var actualX = Cartesian3.fromCartesian4(Matrix4.getColumn(returnedResult, 0, new Cartesian4()));
var actualY = Cartesian3.fromCartesian4(Matrix4.getColumn(returnedResult, 1, new Cartesian4()));
var actualZ = Cartesian3.fromCartesian4(Matrix4.getColumn(returnedResult, 2, new Cartesian4()));
var actualTranslation = Cartesian3.fromCartesian4(Matrix4.getColumn(returnedResult, 3, new Cartesian4()));

expect(actualX).toEqual(expectedX);
expect(actualY).toEqual(expectedY);
expect(actualZ).toEqual(expectedZ);
expect(actualTranslation).toEqual(origin);
});

it('aircraftHeadingPitchRollToFixedFrame works with a result parameter', function() {
var origin = new Cartesian3(1.0, 0.0, 0.0);
var heading = CesiumMath.toRadians(20.0);
var pitch = CesiumMath.toRadians(30.0);
var roll = CesiumMath.toRadians(40.0);

var expectedRotation = Matrix3.fromQuaternion(Quaternion.fromHeadingPitchRoll(heading, pitch, roll));
var expectedX = Matrix3.getColumn(expectedRotation, 0, new Cartesian3());
var expectedY = Matrix3.getColumn(expectedRotation, 1, new Cartesian3());
var expectedZ = Matrix3.getColumn(expectedRotation, 2, new Cartesian3());

Cartesian3.fromElements(-expectedX.z, expectedX.y, expectedX.x, expectedX);
Cartesian3.fromElements(-expectedY.z, expectedY.y, expectedY.x, expectedY);
Cartesian3.fromElements(-expectedZ.z, expectedZ.y, expectedZ.x, expectedZ);

var result = new Matrix4();
var returnedResult = Transforms.aircraftHeadingPitchRollToFixedFrame(origin, heading, pitch, roll, Ellipsoid.UNIT_SPHERE, result);
var actualX = Cartesian3.fromCartesian4(Matrix4.getColumn(returnedResult, 0, new Cartesian4()));
var actualY = Cartesian3.fromCartesian4(Matrix4.getColumn(returnedResult, 1, new Cartesian4()));
var actualZ = Cartesian3.fromCartesian4(Matrix4.getColumn(returnedResult, 2, new Cartesian4()));
var actualTranslation = Cartesian3.fromCartesian4(Matrix4.getColumn(returnedResult, 3, new Cartesian4()));

expect(returnedResult).toBe(result);
expect(actualX).toEqual(expectedX);
expect(actualY).toEqual(expectedY);
expect(actualZ).toEqual(expectedZ);
expect(actualTranslation).toEqual(origin);
});

it('headingPitchRollQuaternion works without a result parameter', function() {
var origin = new Cartesian3(1.0, 0.0, 0.0);
var heading = CesiumMath.toRadians(20.0);
Expand Down Expand Up @@ -273,6 +329,36 @@ defineSuite([
expect(actual).toEqualEpsilon(expected, CesiumMath.EPSILON11);
});

it('aircraftHeadingPitchRollQuaternion works without a result parameter', function() {
var origin = new Cartesian3(1.0, 0.0, 0.0);
var heading = CesiumMath.toRadians(20.0);
var pitch = CesiumMath.toRadians(30.0);
var roll = CesiumMath.toRadians(40.0);

var transform = Transforms.aircraftHeadingPitchRollToFixedFrame(origin, heading, pitch, roll, Ellipsoid.UNIT_SPHERE);
var expected = Matrix4.getRotation(transform, new Matrix3());

var quaternion = Transforms.aircraftHeadingPitchRollQuaternion(origin, heading, pitch, roll, Ellipsoid.UNIT_SPHERE);
var actual = Matrix3.fromQuaternion(quaternion);
expect(actual).toEqualEpsilon(expected, CesiumMath.EPSILON11);
});

it('aircraftHeadingPitchRollQuaternion works with a result parameter', function() {
var origin = new Cartesian3(1.0, 0.0, 0.0);
var heading = CesiumMath.toRadians(20.0);
var pitch = CesiumMath.toRadians(30.0);
var roll = CesiumMath.toRadians(40.0);

var transform = Transforms.aircraftHeadingPitchRollToFixedFrame(origin, heading, pitch, roll, Ellipsoid.UNIT_SPHERE);
var expected = Matrix4.getRotation(transform, new Matrix3());

var result = new Quaternion();
var quaternion = Transforms.aircraftHeadingPitchRollQuaternion(origin, heading, pitch, roll, Ellipsoid.UNIT_SPHERE, result);
var actual = Matrix3.fromQuaternion(quaternion);
expect(quaternion).toBe(result);
expect(actual).toEqualEpsilon(expected, CesiumMath.EPSILON11);
});

it('computeTemeToPseudoFixedMatrix works before noon', function() {
var time = JulianDate.fromDate(new Date('June 29, 2015 12:00:00 UTC'));
var t = Transforms.computeTemeToPseudoFixedMatrix(time);
Expand Down Expand Up @@ -795,6 +881,54 @@ defineSuite([
}).toThrowDeveloperError();
});

it('aircraftHeadingPitchRollToFixedFrame throws without an origin', function() {
expect(function() {
Transforms.aircraftHeadingPitchRollToFixedFrame(undefined, 0.0, 0.0, 0.0);
}).toThrowDeveloperError();
});

it('aircraftHeadingPitchRollToFixedFrame throws without an heading', function() {
expect(function() {
Transforms.aircraftHeadingPitchRollToFixedFrame(Cartesian3.ZERO, undefined, 0.0, 0.0);
}).toThrowDeveloperError();
});

it('aircraftHeadingPitchRollToFixedFrame throws without an pitch', function() {
expect(function() {
Transforms.aircraftHeadingPitchRollToFixedFrame(Cartesian3.ZERO, 0.0, undefined, 0.0);
}).toThrowDeveloperError();
});

it('aircraftHeadingPitchRollToFixedFrame throws without an roll', function() {
expect(function() {
Transforms.aircraftHeadingPitchRollToFixedFrame(Cartesian3.ZERO, 0.0, 0.0, undefined);
}).toThrowDeveloperError();
});

it('aircraftHeadingPitchRollQuaternion throws without an origin', function() {
expect(function() {
Transforms.aircraftHeadingPitchRollQuaternion(undefined, 0.0, 0.0, 0.0);
}).toThrowDeveloperError();
});

it('aircraftHeadingPitchRollQuaternion throws without an heading', function() {
expect(function() {
Transforms.aircraftHeadingPitchRollQuaternion(Cartesian3.ZERO, undefined, 0.0, 0.0);
}).toThrowDeveloperError();
});

it('aircraftHeadingPitchRollQuaternion throws without an pitch', function() {
expect(function() {
Transforms.aircraftHeadingPitchRollQuaternion(Cartesian3.ZERO, 0.0, undefined, 0.0);
}).toThrowDeveloperError();
});

it('aircraftHeadingPitchRollQuaternion throws without an roll', function() {
expect(function() {
Transforms.aircraftHeadingPitchRollQuaternion(Cartesian3.ZERO, 0.0, 0.0, undefined);
}).toThrowDeveloperError();
});

it('computeTemeToPseudoFixedMatrix throws without a date', function() {
expect(function() {
Transforms.computeTemeToPseudoFixedMatrix(undefined);
Expand Down