# Direction Cosine Matrix ECI to ECEF

Convert Earth-centered inertial (ECI) to Earth-centered Earth-fixed (ECEF) coordinates

**Libraries:**

Aerospace Blockset /
Utilities /
Axes Transformations

## Description

The Direction Cosine Matrix ECI to ECEF block calculates the position direction cosine matrix ( Earth-centered inertial to Earth-centered Earth-fixed ), based on the specified reduction method and Coordinated Universal Time (UTC), for the specified time and geophysical data.

## Ports

### Input

**ΔUT1** — Difference between UTC and Universal Time

scalar

Difference between UTC and Universal Time (UT1) in seconds, specified as a scalar, for which the function calculates the direction cosine or transformation matrix.

**Example: **
`0.234`

#### Dependencies

To enable this port, select the **Higher accuracy parameters** check
box.

**Data Types: **`double`

**ΔAT** — Difference between International Atomic Time and UTC

scalar

Difference between International Atomic Time (IAT) and UTC, specified as a scalar, in seconds, for which the function calculates the direction cosine or transformation matrix.

**Example: **
`32`

#### Dependencies

To enable this port, select the **Higher accuracy parameters** check
box.

**Data Types: **`double`

**[xp,yp]** — Polar displacement of Earth

1-by-2 array

Polar displacement of Earth, specified as a 1-by-2 array, in radians, from the motion of
the Earth crust, along the *x*-axis and
*y*-axis.

**Example: **
`[-0.0682e-5 0.1616e-5]`

#### Dependencies

To enable this port, select the **Higher accuracy parameters** check
box.

**Data Types: **`double`

**Port_5** — Adjustment based on reduction method

1-by-2 array

Adjustment based on reduction method, specified as 1-by-2 array. The
name of the port depends on the setting of the
**Reduction** parameter:

If the reduction method is

`IAU-2000/2006`

, this input is the adjustment to the location of the Celestial Intermediate Pole (CIP), specified in radians. This location ([d*X*, d*Y*]) is along the*x*-axis and*y*-axis.If the reduction method is

`IAU-76/FK5`

, this input is the adjustment to the longitude ([Δδψ, Δδε]), specified in radians.

For historical values, see the International Earth Rotation and Reference Systems
Service website (`https://www.iers.org`

).

**Example: **
`[-0.2530e-6 -0.0188e-6]`

#### Dependencies

To enable this port, select the **Higher accuracy
parameters** check box.

**Data Types: **`double`

**Port_6** — Time increment source

scalar

Time increment source, specified as a scalar, such as the Clock block.

#### Dependencies

The port name and time increment depend on the

**Time Increment**parameter.**Time Increment**ValuePort Name `Day`

**day**`Hour`

**hour**`Min`

**min**`Sec`

**sec**`None`

No port

To disable this port, set the

**Time Increment**parameter to`None`

.

**Data Types: **`double`

### Output

**DCM**_{fi} — Direction cosine matrix

3-by-3 matrix

_{fi}

Direction cosine matrix ECI to ECEF.

**Data Types: **`double`

## Parameters

**Reduction** — Reduction method

`IAU-76/FK5`

(default) | `IAU-2000/2006`

Reduction method to calculate the direction cosine matrix. The method can be one of the following:

`IAU-76/FK5`

Reduce the calculation using the IAU-76/Fifth Fundamental Catalogue (FK5) reference system. Choose this reduction method if the reference coordinate system for the conversion is FK5.

**Note**This method uses the IAU 1976 precession model and the IAU 1980 theory of nutation to reduce the calculation. This model and theory are no longer current, but the software provides this reduction method for existing implementations. Because of the polar motion approximation that this reduction method uses, the block calculates the transformation matrix rather than the direction cosine matrix.

`IAU-2000/2006`

Reduce the calculation using the International Astronomical Union (IAU)-2000/2006 reference system. Choose this reduction method if the reference coordinate system for the conversion is IAU-2000. This reduction method uses the P03 precession model to reduce the calculation.

#### Programmatic Use

Block Parameter:
`red` |

Type: character vector |

Values:
`'IAU-2000/2006'` |
`'IAU-76/FK5'` |

Default:
`'IAU-2000/2006'` |

**Year** — Year

`2013`

(default) | double, whole number, greater than 1

Year to calculate the Coordinated Universal Time (UTC) date. Enter a double value that is
a whole number greater than 1, such as `2013`

.

#### Programmatic Use

Block Parameter:
`year` |

Type: character vector |

Values: double, whole number,
greater than 1 |

Default:
`'2013'` |

**Month** — Month

`January`

(default) | `February`

| `March`

| `April`

| `May`

| `June`

| `July`

| `August`

| `September`

| `October`

| `November`

| `December`

Month to calculate the UTC date.

#### Programmatic Use

Block Parameter:
`month` |

Type: character vector |

Values:
`'January'` | `'February'` |
`'March'` | `'April'` |
`'May'` | `'June'` |
`'July'` | `'August'` |
`'September'` | `'October'` |
`'November'` |
`'December'` |

Default:
`'January'` |

**Day** — Day

`1`

(default) | `2`

| `3`

| `4`

| `5`

| `6`

| `7`

| `8`

| `9`

| `10`

| `11`

| `12`

| `13`

| `14`

| `15`

| `16`

| `17`

| `18`

| `19`

| `20`

| `21`

| `22`

| `23`

| `24`

| `25`

| `26`

| `27`

| `28`

| `29`

| `30`

| `31`

Day to calculate the UTC date.

#### Programmatic Use

Block Parameter:
`day` |

Type: character vector |

Values: `'1'`
| `'2'` | `'3'` |
`'4'` | `'5'` |
`'6'` | `'7'` |
`'8'` | `'9'` |
`'10'` | `'11'` |
`'12'` | `'13'` |
`'14'` | `'15'` |
`'16'` | `'17'` |
`'18'` | `'19'` |
`'20'` | `'21'` |
`'22'` | `'23'` |
`'24'` | `'25'` |
`'26'` | `'27'` |
`'28'` | `'29'` |
`'30'` | `'31'` |

Default:
`'1'` |

**Hour** — Hour

`0`

(default) | double, whole number, in the range of `0`

and
`24`

Hour to calculate the UTC date. Enter a double value that is a whole
number, from `0`

to `24`

.

#### Programmatic Use

Block Parameter:
`hour` |

Type: character vector |

Values: double, whole number,
`0` to `24` |

Default:
`'0'` |

**Minutes** — Minutes

`0`

(default) | double, whole number, in the range of `0`

and
`60`

Minutes to calculate the UTC date. Enter a double value that is a whole
number, from `0`

to `60`

.

#### Programmatic Use

Block Parameter:
`min` |

Type: character vector |

Values: double, whole number,
`0` to `60` |

Default:
`'0'` |

**Seconds** — Seconds

`0`

(default) | double, whole number, in the range of `0`

and
`60`

Seconds to calculate the UTC date. Enter a double value that is a whole
number, from `0`

to `60`

.

#### Programmatic Use

Block Parameter:
`sec` |

Type: character vector |

Values: double, whole number,
`0` to `60` |

Default:
`'0'` |

**Time increment** — Time increment

`Day`

(default) | `Hour`

| `Min`

| `Sec`

| `None`

Time increment between the specified date and the desired model simulation
time. The block adjusts the calculated direction cosine matrix to take into
account the time increment from model simulation. For example, selecting
`Day`

and connecting a simulation timer to the port
means that each time increment unit is one day and the block adjusts its
calculation based on that simulation time.

This parameter corresponds to the time increment input, the clock source.

If you select `None`

, the calculated Julian date does not
take into account the model simulation time.

#### Programmatic Use

Block Parameter:
`deltaT` |

Type: character vector |

Values:
`'None'` | `'Day'` |
`'Hour'` | `'Min'` |
`'Sec'` |

Default:
`'Day'` |

**Action for out-of-range input** — Out-of-range block behavior

`None`

(default) | `Warning`

| `Error`

Out-of-range block behavior, specified as follows.

Action | Description |
---|---|

| No action. |

| Warning in the Diagnostic Viewer, model simulation continues. |

| Error in the Diagnostic Viewer, model simulation stops. |

#### Programmatic Use

Block Parameter: `errorflag` |

Type: character vector |

Values: `'None'` | `'Warning'` | `'Error'` |

Default: `'Error'` |

**Higher accuracy parameters** — Enable higher accuracy parameters

`on`

(default) | `off`

Select this check box to enable these inputs. These inputs let you better control the conversion result. See Input for a description.

Δ

*UT1*Δ

*AT*[

*xp*,*yp*][Δδψ, Δδε] or [d

*X*, d*Y*]

#### Programmatic Use

Block Parameter:
`extraparamflag` |

Type: character vector |

Values: `'on'`
| `'off'` |

Default:
`'on'` |

## Extended Capabilities

### C/C++ Code Generation

Generate C and C++ code using Simulink® Coder™.

## Version History

**Introduced in R2013b**

## MATLAB 명령

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