MunitionModel (Autonomous Unmanned Vehicle (AUV) Workbench Documentation)

java.lang.Object
- dynamics.models.munition.MunitionModel

public class MunitionModel
extends Object

Field Summary

Fields
Modifier and Type	Field and Description
`protected double`	`Clp` Nose roll damping coeff. (1/s)
`protected double`	`Cma` Aero restoring momentum slope coeff.
`protected double`	`CNa` Aero normal force slope coeff. wrt beta (second/meter2)
`protected double`	`CX0` Aero coeff.
`protected double`	`CXa2` Aero coeff.
`protected double`	`Cypa` Aero Magnus force slope coeff. wrt beta and (p*D/2V) (1/rad)
`protected double`	`D` Projectile diameter (m)
`protected double`	`delFin` 1 degree Tail fin cant (radians)
`protected double`	`gE` Gun elevation from surface (degrees)
`protected double`	`gH` Gun height from sea level (meter)
`protected double`	`lx` Polar moment of inertia (kg/m2)
`protected double`	`massBurnRate` Rocket booster mass burn rate (kilogram/second)
`protected double`	`massBurnTime` seconds
`protected double`	`rbV` Rocket Boost Velocity - (meter/second)
`protected double`	`rocketBoostAcceleration` N or kg-m/s2
`protected double`	`rocketBoostIgnitionTime` (second)
`protected double`	`S` Surface area (m2)

Constructor Summary

Constructors
Constructor and Description

MunitionModel()

Constructors
Constructor and Description
`MunitionModel()`

Method Summary

Methods
Modifier and Type Method and Description

void load(String fileName)
Loads coefficients from an XML configuration file

static void main(String[] args)
- Methods inherited from class java.lang.Object
  clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods
Modifier and Type	Method and Description
`void`	`load(String fileName)` Loads coefficients from an XML configuration file
`static void`	`main(String[] args)`

- Field Detail
  - lx
```
protected double lx
```
    Polar moment of inertia (kg/m2)
  - S
```
protected double S
```
    Surface area (m2)
  - D
```
protected double D
```
    Projectile diameter (m)
  - CX0
```
protected double CX0
```
    Aero coeff. (m/s)
  - CXa2
```
protected double CXa2
```
    Aero coeff. (ms2/rad2)
  - Clp
```
protected double Clp
```
    Nose roll damping coeff. (1/s)
  - CNa
```
protected double CNa
```
    Aero normal force slope coeff. wrt beta (second/meter2)
  - Cma
```
protected double Cma
```
    Aero restoring momentum slope coeff. (m3/rad)
  - Cypa
```
protected double Cypa
```
    Aero Magnus force slope coeff. wrt beta and (p*D/2V) (1/rad)
  - gH
```
protected double gH
```
    Gun height from sea level (meter)
  - gE
```
protected double gE
```
    Gun elevation from surface (degrees)
  - rbV
```
protected double rbV
```
    Rocket Boost Velocity - (meter/second)
  - delFin
```
protected double delFin
```
    1 degree Tail fin cant (radians)
  - rocketBoostAcceleration
```
protected double rocketBoostAcceleration
```
    N or kg-m/s2
  - massBurnRate
```
protected double massBurnRate
```
    Rocket booster mass burn rate (kilogram/second)
  - rocketBoostIgnitionTime
```
protected double rocketBoostIgnitionTime
```
    (second)
  - massBurnTime
```
protected double massBurnTime
```
    seconds
- Constructor Detail
  - MunitionModel
```
public MunitionModel()
```
- Method Detail
  - load
```
public void load(String fileName)
```
    Loads coefficients from an XML configuration file
  - main
```
public static void main(String[] args)
```

Class MunitionModel

Field Summary

Constructor Summary

Method Summary

Methods inherited from class java.lang.Object

Field Detail

lx

S

D

CX0

CXa2

Clp

CNa

Cma

Cypa

gH

gE

rbV

delFin

rocketBoostAcceleration

massBurnRate

rocketBoostIgnitionTime

massBurnTime

Constructor Detail

MunitionModel

Method Detail

load

main