OrbitManeuver (OREKIT 12.0.1 API)

java.lang.Object
- org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

All Implemented Interfaces:

TimeStamped
```
public class OrbitManeuver
extends Object
implements TimeStamped
```
Maneuver entry.

Since:

11.0

Author:

Luc Maisonobe

Constructor Summary

Constructors
Constructor and Description
`OrbitManeuver()` Build an uninitialized maneuver.

Method Summary

All Methods Instance Methods Concrete Methods
Modifier and Type	Method and Description
`org.hipparchus.geometry.euclidean.threed.Vector3D`	`getAcceleration()` Get acceleration.
`double`	`getAccelerationDirectionSigma()` Get one σ angular off-nominal acceleration direction.
`OnOff`	`getAccelerationInterpolation()` Get interpolation mode between current and next acceleration line.
`double`	`getAccelerationMagnitudeSigma()` Get one σ percent error on acceleration magnitude.
`AbsoluteDate`	`getDate()` Get the date.
`double`	`getDeltaMass()` Get mass change.
`double`	`getDeployDirSigma()` Get one σ angular off-nominal deployment vector direction.
`org.hipparchus.geometry.euclidean.threed.Vector3D`	`getDeployDv()` Get velocity increment of deployed "child" object.
`double`	`getDeployDvCda()` Get typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
`double`	`getDeployDvRatio()` Get ratio of child-to-host ΔV vectors.
`double`	`getDeployDvSigma()` Get one σ percent error on deployment ΔV magnitude.
`String`	`getDeployId()` Get identifier of resulting "child" object deployed from this host.
`double`	`getDeployMass()` Get decrement in host mass as a result of deployment.
`double`	`getDuration()` Get duration.
`org.hipparchus.geometry.euclidean.threed.Vector3D`	`getDv()` Get velocity increment.
`double`	`getDvDirSigma()` Get one σ angular off-nominal ΔV direction.
`double`	`getDvMagSigma()` Get one σ percent error on ΔV magnitude.
`org.hipparchus.geometry.euclidean.threed.Vector3D`	`getThrust()` Get thrust.
`double`	`getThrustDirectionSigma()` Get one σ angular off-nominal thrust direction.
`double`	`getThrustEfficiency()` Get thrust efficiency η.
`OnOff`	`getThrustInterpolation()` Get interpolation mode between current and next thrust line.
`double`	`getThrustIsp()` Get thrust specific impulse.
`double`	`getThrustMagnitudeSigma()` Get one σ percent error on thrust magnitude.
`void`	`setAcceleration(int i, double ai)` Set acceleration component.
`void`	`setAccelerationDirectionSigma(double accelerationDirectionSigma)` Set one σ angular off-nominal acceleration direction.
`void`	`setAccelerationInterpolation(OnOff accelerationInterpolation)` Set interpolation mode between current and next acceleration line.
`void`	`setAccelerationMagnitudeSigma(double accelerationMagnitudeSigma)` Set one σ percent error on acceleration magnitude.
`void`	`setDate(AbsoluteDate date)` Set date.
`void`	`setDeltaMass(double deltaMass)` Set mass change.
`void`	`setDeployDirSigma(double deployDirSigma)` Set one σ angular off-nominal deployment vector direction.
`void`	`setDeployDv(int i, double deployDvi)` Set velocity increment component of deployed "child" object.
`void`	`setDeployDvCda(double deployDvCda)` Set typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
`void`	`setDeployDvRatio(double deployDvRatio)` Set ratio of child-to-host ΔV vectors.
`void`	`setDeployDvSigma(double deployDvSigma)` Set one σ percent error on deployment ΔV magnitude.
`void`	`setDeployId(String deployId)` Set identifier of resulting "child" object deployed from this host.
`void`	`setDeployMass(double deployMass)` Set decrement in host mass as a result of deployment.
`void`	`setDuration(double duration)` Set duration.
`void`	`setDv(int i, double dVi)` Set velocity increment component.
`void`	`setDvDirSigma(double dvDirSigma)` Set one σ angular off-nominal ΔV direction.
`void`	`setDvMagSigma(double dvMagSigma)` Set one σ percent error on ΔV magnitude.
`void`	`setThrust(int i, double ti)` Set thrust component.
`void`	`setThrustDirectionSigma(double thrustDirectionSigma)` Set one σ angular off-nominal thrust direction.
`void`	`setThrustEfficiency(double thrustEfficiency)` Set thrust efficiency η.
`void`	`setThrustInterpolation(OnOff thrustInterpolation)` Set interpolation mode between current and next thrust line.
`void`	`setThrustIsp(double thrustIsp)` Set thrust specific impulse.
`void`	`setThrustMagnitudeSigma(double thrustMagnitudeSigma)` Set one σ percent error on thrust magnitude.

Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.time.TimeStamped
durationFrom

- Constructor Detail
  - OrbitManeuver
```
public OrbitManeuver()
```
    Build an uninitialized maneuver.
- Method Detail
  - getDate
```
public AbsoluteDate getDate()
```
    Get the date.
    
    Specified by:
    
    getDate in interface TimeStamped
    
    Returns:
    
    date attached to the object
  - setDate
```
public void setDate(AbsoluteDate date)
```
    Set date.
    
    Parameters:
    
    date - maneuver date
  - getDuration
```
public double getDuration()
```
    Get duration.
    
    Returns:
    
    duration
  - setDuration
```
public void setDuration(double duration)
```
    Set duration.
    
    Parameters:
    
    duration - duration
  - getDeltaMass
```
public double getDeltaMass()
```
    Get mass change.
    
    Returns:
    
    mass change
  - setDeltaMass
```
public void setDeltaMass(double deltaMass)
```
    Set mass change.
    
    Parameters:
    
    deltaMass - mass change
  - getAcceleration
```
public org.hipparchus.geometry.euclidean.threed.Vector3D getAcceleration()
```
    Get acceleration.
    
    Returns:
    
    acceleration
  - setAcceleration
```
public void setAcceleration(int i,
                            double ai)
```
    Set acceleration component.
    
    Parameters:
    
    i - component index
    
    ai - i^th component of acceleration
  - getAccelerationInterpolation
```
public OnOff getAccelerationInterpolation()
```
    Get interpolation mode between current and next acceleration line.
    
    Returns:
    
    interpolation mode between current and next acceleration line
  - setAccelerationInterpolation
```
public void setAccelerationInterpolation(OnOff accelerationInterpolation)
```
    Set interpolation mode between current and next acceleration line.
    
    Parameters:
    
    accelerationInterpolation - interpolation mode between current and next acceleration line
  - getAccelerationMagnitudeSigma
```
public double getAccelerationMagnitudeSigma()
```
    Get one σ percent error on acceleration magnitude.
    
    Returns:
    
    one σ percent error on acceleration magnitude
  - setAccelerationMagnitudeSigma
```
public void setAccelerationMagnitudeSigma(double accelerationMagnitudeSigma)
```
    Set one σ percent error on acceleration magnitude.
    
    Parameters:
    
    accelerationMagnitudeSigma - one σ percent error on acceleration magnitude
  - getAccelerationDirectionSigma
```
public double getAccelerationDirectionSigma()
```
    Get one σ angular off-nominal acceleration direction.
    
    Returns:
    
    one σ angular off-nominal acceleration direction
  - setAccelerationDirectionSigma
```
public void setAccelerationDirectionSigma(double accelerationDirectionSigma)
```
    Set one σ angular off-nominal acceleration direction.
    
    Parameters:
    
    accelerationDirectionSigma - one σ angular off-nominal acceleration direction
  - getDv
```
public org.hipparchus.geometry.euclidean.threed.Vector3D getDv()
```
    Get velocity increment.
    
    Returns:
    
    velocity increment
  - setDv
```
public void setDv(int i,
                  double dVi)
```
    Set velocity increment component.
    
    Parameters:
    
    i - component index
    
    dVi - i^th component of velocity increment
  - getDvMagSigma
```
public double getDvMagSigma()
```
    Get one σ percent error on ΔV magnitude.
    
    Returns:
    
    one σ percent error on ΔV magnitude
  - setDvMagSigma
```
public void setDvMagSigma(double dvMagSigma)
```
    Set one σ percent error on ΔV magnitude.
    
    Parameters:
    
    dvMagSigma - one σ percent error on ΔV magnitude
  - getDvDirSigma
```
public double getDvDirSigma()
```
    Get one σ angular off-nominal ΔV direction.
    
    Returns:
    
    one σ angular off-nominal ΔV direction
  - setDvDirSigma
```
public void setDvDirSigma(double dvDirSigma)
```
    Set one σ angular off-nominal ΔV direction.
    
    Parameters:
    
    dvDirSigma - one σ angular off-nominal ΔV direction
  - getThrust
```
public org.hipparchus.geometry.euclidean.threed.Vector3D getThrust()
```
    Get thrust.
    
    Returns:
    
    thrust
  - setThrust
```
public void setThrust(int i,
                      double ti)
```
    Set thrust component.
    
    Parameters:
    
    i - component index
    
    ti - i^th component of thrust
  - getThrustEfficiency
```
public double getThrustEfficiency()
```
    Get thrust efficiency η.
    
    Returns:
    
    thrust efficiency η (typically between 0.0 and 1.0)
  - setThrustEfficiency
```
public void setThrustEfficiency(double thrustEfficiency)
```
    Set thrust efficiency η.
    
    Parameters:
    
    thrustEfficiency - thrust efficiency η (typically between 0.0 and 1.0)
  - getThrustInterpolation
```
public OnOff getThrustInterpolation()
```
    Get interpolation mode between current and next thrust line.
    
    Returns:
    
    interpolation mode between current and next thrust line
  - setThrustInterpolation
```
public void setThrustInterpolation(OnOff thrustInterpolation)
```
    Set interpolation mode between current and next thrust line.
    
    Parameters:
    
    thrustInterpolation - interpolation mode between current and next thrust line
  - getThrustIsp
```
public double getThrustIsp()
```
    Get thrust specific impulse.
    
    Returns:
    
    thrust specific impulse
  - setThrustIsp
```
public void setThrustIsp(double thrustIsp)
```
    Set thrust specific impulse.
    
    Parameters:
    
    thrustIsp - thrust specific impulse
  - getThrustMagnitudeSigma
```
public double getThrustMagnitudeSigma()
```
    Get one σ percent error on thrust magnitude.
    
    Returns:
    
    one σ percent error on thrust magnitude
  - setThrustMagnitudeSigma
```
public void setThrustMagnitudeSigma(double thrustMagnitudeSigma)
```
    Set one σ percent error on thrust magnitude.
    
    Parameters:
    
    thrustMagnitudeSigma - one σ percent error on thrust magnitude
  - getThrustDirectionSigma
```
public double getThrustDirectionSigma()
```
    Get one σ angular off-nominal thrust direction.
    
    Returns:
    
    one σ angular off-nominal thrust direction
  - setThrustDirectionSigma
```
public void setThrustDirectionSigma(double thrustDirectionSigma)
```
    Set one σ angular off-nominal thrust direction.
    
    Parameters:
    
    thrustDirectionSigma - one σ angular off-nominal thrust direction
  - getDeployId
```
public String getDeployId()
```
    Get identifier of resulting "child" object deployed from this host.
    
    Returns:
    
    identifier of resulting "child" object deployed from this host
  - setDeployId
```
public void setDeployId(String deployId)
```
    Set identifier of resulting "child" object deployed from this host.
    
    Parameters:
    
    deployId - identifier of resulting "child" object deployed from this host
  - getDeployDv
```
public org.hipparchus.geometry.euclidean.threed.Vector3D getDeployDv()
```
    Get velocity increment of deployed "child" object.
    
    Returns:
    
    velocity increment of deployed "child" object
  - setDeployDv
```
public void setDeployDv(int i,
                        double deployDvi)
```
    Set velocity increment component of deployed "child" object.
    
    参数:
    
    i - 组件索引
    
    deployDvi - 部署的“子”对象速度增量的第i个分量
  - getDeployMass
```
public double getDeployMass()
```
    获取部署导致的主体质量减少。
    
    返回:
    
    部署导致的主体质量减少（应≤ 0）
  - setDeployMass
```
public void setDeployMass(double deployMass)
```
    设置部署导致的主体质量减少。
    
    参数:
    
    deployMass - 部署导致的主体质量减少（应≤ 0）
  - getDeployDvSigma
```
public double getDeployDvSigma()
```
    获取部署ΔV大小的一σ百分比误差。
    
    返回:
    
    部署ΔV大小的一σ百分比误差
  - setDeployDvSigma
```
public void setDeployDvSigma(double deployDvSigma)
```
    设置部署ΔV大小的一σ百分比误差。
    
    参数:
    
    deployDvSigma - 部署ΔV大小的一σ百分比误差
  - getDeployDirSigma
```
public double getDeployDirSigma()
```
    获取一σ非标称部署矢量方向。
    
    返回:
    
    一σ非标称部署矢量方向
  - setDeployDirSigma
```
public void setDeployDirSigma(double deployDirSigma)
```
    设置一σ非标称部署矢量方向。
    
    参数:
    
    deployDirSigma - 一σ非标称部署矢量方向
  - getDeployDvRatio
```
public double getDeployDvRatio()
```
    获取子体到主体ΔV矢量的比率。
    
    返回:
    
    子体到主体ΔV矢量的比率
  - setDeployDvRatio
```
public void setDeployDvRatio(double deployDvRatio)
```
    设置子体到主体ΔV矢量的比率。
    
    参数:
    
    deployDvRatio - 子体到主体ΔV矢量的比率
  - getDeployDvCda
```
public double getDeployDvCda()
```
    获取部署的“子”对象阻力系数乘以横截面积的典型（50th percentile）乘积。
    
    返回:
    
    部署的“子”对象阻力系数乘以横截面积的典型（50th percentile）乘积
  - setDeployDvCda
```
public void setDeployDvCda(double deployDvCda)
```
    设置部署的“子”对象阻力系数乘以横截面积的典型（50th percentile）乘积。
    
    参数:
    
    deployDvCda - 部署的“子”对象阻力系数乘以横截面积的典型（50th percentile）乘积

Class OrbitManeuver

Constructor Summary

Method Summary

Methods inherited from class java.lang.Object

Methods inherited from interface org.orekit.time.TimeStamped

Constructor Detail

OrbitManeuver

Method Detail

getDate

setDate

getDuration

setDuration

getDeltaMass

setDeltaMass

getAcceleration

setAcceleration

getAccelerationInterpolation

setAccelerationInterpolation

getAccelerationMagnitudeSigma

setAccelerationMagnitudeSigma

getAccelerationDirectionSigma

setAccelerationDirectionSigma

getDv

setDv

getDvMagSigma

setDvMagSigma

getDvDirSigma

setDvDirSigma

getThrust

setThrust

getThrustEfficiency

setThrustEfficiency

getThrustInterpolation

setThrustInterpolation

getThrustIsp

setThrustIsp

getThrustMagnitudeSigma

setThrustMagnitudeSigma

getThrustDirectionSigma

setThrustDirectionSigma

getDeployId

setDeployId

getDeployDv

setDeployDv

getDeployMass

setDeployMass

getDeployDvSigma

setDeployDvSigma

getDeployDirSigma

setDeployDirSigma

getDeployDvRatio

setDeployDvRatio

getDeployDvCda

setDeployDvCda