Engee documentation

4th Order Point Mass (Longitudinal) GOST

A model of the plane translational motion of a material point according to GOST 20058-80.

blockType: SubSystem

Path in the library:

/Aerospace/Equations of Motion/Point Mass/4th Order Point Mass (Longitudinal) GOST

Description

Block 4th Order Point Mass (Longitudinal) GOST implements a model of flat translational motion of a material point according to GOST 20058-80.

The equations of motion have the form:







Block 4th Order Point Mass (Longitudinal) GOST it works in SI units.

The block uses coordinate systems according to GOST 20058-80.

Ports

Input

# Fx (N) — projection of the applied force on the axis к
scalar

Details

Projection of the applied force on the axis к trajectory coordinate system, N.

Data types

Float64

Complex numbers support

No

# Fy (N) — projection of the applied force on the axis к
scalar

Details

Projection of the applied force on the axis к trajectory coordinate system, N.

Data types

Float64

Complex numbers support

No

Output

# θ (rad) — trajectory tilt angle
scalar

Details

The angle of the trajectory, rad.

Data types

Float64

Complex numbers support

No

# Vx (m/s) — airspeed
scalar

Details

Air velocity of the material point, m/s.

Data types

Float64

Complex numbers support

No

# X (m) — distance traveled
scalar

Details

Distance traveled, m.

Data types

Float64

Complex numbers support

No

# H (m) — Flight altitude
scalar

Details

Flight altitude, m.

Data types

Float64

Complex numbers support

No

Parameters

Main

# Initial flight path angle — the initial angle of the trajectory

Details

The initial angle of inclination of the trajectory, rad.

Default value

0.0

Program usage name

gamma0

Tunable

No

Evaluatable

Yes

# Initial airspeed — initial airspeed

Details

Initial airspeed, m/s.

Default value

100.0

Program usage name

V0

Tunable

No

Evaluatable

Yes

# Initial downrange [East] — starting position

Details

The initial position of the material point in the moving coordinate system, m.

Default value

0.0

Program usage name

x0

Tunable

No

Evaluatable

Yes

# Initial altitude [Up] — initial flight altitude

Details

Initial flight altitude, m.

Default value

0.0

Program usage name

h0

Tunable

No

Evaluatable

Yes

# Initial mass — weight

Details

Weight, kg.

Default value

1.0

Program usage name

mass0

Tunable

No

Evaluatable

Yes