计算分辨率

This commit is contained in:
nuknal
2024-06-07 13:03:01 +08:00
parent cf5012f2a8
commit c046da2321
6 changed files with 240 additions and 105 deletions

View File

@@ -14,7 +14,13 @@ const (
nPixels = 9344 // 像素数
)
func Intersection(q Quaternion, satPos []float64, satTime time.Time, ucam int) (float64, float64) {
type IntersectionPoint struct {
Lat float64
Lon float64
H float64
}
func Intersection(q Quaternion, satPos84 []float64, satTime time.Time, ucam int) IntersectionPoint {
alpha := FOV * math.Pi / 180.0
alpha = -alpha/2.0 + float64(ucam)*(alpha/float64(nPixels))
direction := []float64{0, math.Tan(alpha), -1.3}
@@ -33,11 +39,42 @@ func Intersection(q Quaternion, satPos []float64, satTime time.Time, ucam int) (
x, y, z := ECItoECEF(eciDirection[0], eciDirection[1], eciDirection[2], satTime)
ecefDirection := []float64{x, y, z}
intersection := intersectWithEllipsoid(satPos, ecefDirection)
lat, lon, _ := ECEFToGeodetic(intersection[0], intersection[1], intersection[2])
intersection := intersectWithEllipsoid(satPos84, ecefDirection)
lat, lon, h := ECEFToGeodetic(intersection[0], intersection[1], intersection[2])
return IntersectionPoint{Lat: lat, Lon: lon, H: h}
return lat, lon
}
func Intersection2(Qsat2orbit, Qorbit2eci Quaternion, satPos84 []float64, satTime time.Time, ucam int) IntersectionPoint {
alpha := FOV * math.Pi / 180.0
alpha = -alpha/2.0 + float64(ucam)*(alpha/float64(nPixels))
direction := []float64{0, math.Tan(alpha), -1.3} // 卫星相机坐标系下CCD成像方向向量
// -------- 转到轨道坐标系 --------
Rsat2orbit := Qsat2orbit.ToRotationMatrix()
Rsat2orbitT := &mat.Dense{}
Rsat2orbitT.Inverse(Rsat2orbit)
var r0 mat.VecDense
r0.MulVec(Rsat2orbit, mat.NewVecDense(3, direction))
dOrbit := r0.RawVector().Data
// -------- 转到ECI坐标系 --------
Rorbit2eci := Qorbit2eci.ToRotationMatrix()
Rorbit2eciT := &mat.Dense{}
Rorbit2eciT.Inverse(Rorbit2eci)
var r1 mat.VecDense
r1.MulVec(Rorbit2eci, mat.NewVecDense(3, dOrbit))
dECI := r1.RawVector().Data
// -------- 转到ECEF坐标系 --------
x, y, z := ECItoECEF(dECI[0], dECI[1], dECI[2], satTime)
dECEF := []float64{x, y, z}
// -------- 计算交点 --------}
intersection := intersectWithEllipsoid(satPos84, dECEF)
lat, lon, h := ECEFToGeodetic(intersection[0], intersection[1], intersection[2])
return IntersectionPoint{Lat: lat, Lon: lon, H: h}
}
// 计算与椭球表面的交点

View File

@@ -1,6 +1,8 @@
package calculator
import (
"math"
"gonum.org/v1/gonum/mat"
)
@@ -18,3 +20,118 @@ func (q Quaternion) ToRotationMatrix() *mat.Dense {
2*x*z - 2*w*y, 2*y*z + 2*w*x, 1 - 2*x*x - 2*y*y,
})
}
// EulerToQuaternion converts Euler angles (yaw, pitch, roll) to a quaternion.
// Assuming the order of rotations is ZYX (yaw-pitch-roll).
func EulerToQuaternion(yaw, pitch, roll float64) Quaternion {
halfYaw := yaw / 2
halfPitch := pitch / 2
halfRoll := roll / 2
cy := math.Cos(halfYaw)
sy := math.Sin(halfYaw)
cp := math.Cos(halfPitch)
sp := math.Sin(halfPitch)
cr := math.Cos(halfRoll)
sr := math.Sin(halfRoll)
q := Quaternion{
W: cy*cp*cr + sy*sp*sr,
X: cy*cp*sr - sy*sp*cr,
Y: sy*cp*sr + cy*sp*cr,
Z: sy*cp*cr - cy*sp*sr,
}
return q
}
// EulerToRotMatrix converts Euler angles (roll, pitch, yaw) to a rotation matrix.
func EulerToRotMatrix(phi, theta, psi float64) *mat.Dense {
// Calculate individual rotation matrices
Rx := mat.NewDense(3, 3, []float64{
1, 0, 0,
0, math.Cos(phi), -math.Sin(phi),
0, math.Sin(phi), math.Cos(phi),
})
Ry := mat.NewDense(3, 3, []float64{
math.Cos(theta), 0, math.Sin(theta),
0, 1, 0,
-math.Sin(theta), 0, math.Cos(theta),
})
Rz := mat.NewDense(3, 3, []float64{
math.Cos(psi), -math.Sin(psi), 0,
math.Sin(psi), math.Cos(psi), 0,
0, 0, 1,
})
// R = Rz * Ry * Rx
RyRx := mat.NewDense(3, 3, nil)
RyRx.Mul(Ry, Rx)
R := mat.NewDense(3, 3, nil)
R.Mul(Rz, RyRx)
return R
}
// RotMatrixToQuaternion converts a rotation matrix to a quaternion.
func RotMatrixToQuaternion(R *mat.Dense) Quaternion {
m := R.RawMatrix().Data
trace := m[0] + m[4] + m[8]
var q Quaternion
if trace > 0 {
S := 0.5 / math.Sqrt(trace+1.0)
q.W = 0.25 / S
q.X = (m[7] - m[5]) * S
q.Y = (m[2] - m[6]) * S
q.Z = (m[3] - m[1]) * S
} else {
if m[0] > m[4] && m[0] > m[8] {
S := 2.0 * math.Sqrt(1.0+m[0]-m[4]-m[8])
q.W = (m[7] - m[5]) / S
q.X = 0.25 * S
q.Y = (m[1] + m[3]) / S
q.Z = (m[2] + m[6]) / S
} else if m[4] > m[8] {
S := 2.0 * math.Sqrt(1.0+m[4]-m[0]-m[8])
q.W = (m[2] - m[6]) / S
q.X = (m[1] + m[3]) / S
q.Y = 0.25 * S
q.Z = (m[5] + m[7]) / S
} else {
S := 2.0 * math.Sqrt(1.0+m[8]-m[0]-m[4])
q.W = (m[3] - m[1]) / S
q.X = (m[2] + m[6]) / S
q.Y = (m[5] + m[7]) / S
q.Z = 0.25 * S
}
}
return q
}
func RotMatrixToEuler(R *mat.Dense) (yaw, pitch, roll float64) {
m := R.RawMatrix().Data
if m[6] < 1 {
if m[6] > -1 {
pitch = math.Asin(-m[6])
roll = math.Atan2(m[7], m[8])
yaw = math.Atan2(m[3], m[0])
} else {
pitch = math.Pi / 2
roll = -math.Atan2(-m[1], m[4])
yaw = 0
}
} else {
pitch = -math.Pi / 2
roll = math.Atan2(-m[1], m[4])
yaw = 0
}
return yaw, pitch, roll
}