ISO RUS Converter
Translation of physical quantities from ISO 1151-1:1988 to GOST 20058-80.
Description
Block ISO RUS Converter implements the translation of various physical quantities from one reference frame to another, in accordance with GOST 20058-80 (Aircraft dynamics in the atmosphere) and ISO 1151-1:1988 (Flight dynamics - Concepts, quantities and symbols - Part 1: Aircraft motion relative to the air).
Ports
Input
#
ϕ θ ψ
—
input port
vector
Details
The input port to which data is fed according to ISO 1151-1:1988.
Variables that are input to the input port are determined by the value of the parameters Variables.
Data types |
|
Complex numbers support |
No |
Output
#
ϑ γ ψ
—
output port
vector
Details
Output port from which data converted according to GOST 20058-80 is returned.
Variables that are returned from the output port are determined by the value of the parameters Variables.
Data types |
|
Complex numbers support |
No |
Parameters
Parameters
#
Variables —
variables
Euler angles
| Wind angles
| Flight path angles
| Wind direction angles
| Coordinates
| Angular rates
| Velocities
| Angular accelerations
| Accelerations
| Resultant force
| Aerodynamic force
| Moments
| G forces
| Force coefficients
| Moment coefficients
Details
Select the variables to be converted.
Options to select:
-
Euler angles
- Euler angles: roll, pitch, yaw; -
Wind angles
- Euler angles in velocity coordinate system: roll, pitch, yaw; -
Flgiht path angles
- trajectory angles: track angle, climb angle; -
Wind direction angles
- wind velocity vector angles: wind angle, wind slope; -
Angular rates
- angular velocities of the aircraft: roll, pitch, yaw; -
Velocities
- aircraft velocities; -
Resultant force
- resultant force; -
Moments
- moments; -
G forces
- overloads; -
Angular accelerations
- angular accelerations; -
Accelerations
- linear accelerations; -
Moment coefficients
- moment coefficients; -
Aerodynamic force
- aerodynamic force; -
Force coefficients
- force coefficients.
Values |
|
Default value |
|
Program usage name |
|
Tunable |
No |
Evaluatable |
Yes |