Name
|
Description
|
Attributes
|
BCS_X
|
The component of the thrust vector to apply in the Spacecraft BCS X-direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
BCS_Y
|
The component of the thrust vector to apply in the Spacecraft BCS Y-direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
BCS_Z
|
The component of the thrust vector to apply in the Spacecraft BCS Z-direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
BiNormalDirection
|
The component of the thrust vector to apply in the Orbit-BiNormal direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
CoVelocityDirection
|
The component of the thrust vector to apply in the Co-Velocity direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
CrossDirection
|
The component of the thrust vector to apply in the Y cross Z direction of the Geodetic frame.
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
EarthNormalDirection
|
The component of the thrust vector to apply in the Intersection Normal to the Earth's Surface direction.
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
GeoNegativeNormalDirection
|
The component of the thrust vector to apply in the Negative Orbit Normal direction.
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
NadirDirection
|
The component of the thrust vector to apply in the Nadir direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
NegativeNormalDirection
|
The component of the thrust vector to apply in the Negative Orbit-Normal direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
NormalDirection
|
The component of the thrust vector to apply in the Orbit Normal direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
U_PositionDirection
|
The component of the thrust vector to apply in the Position direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
V_VelocityDirection
|
The component of the thrust vector to apply in the Velocity direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
VelocityDirection
|
The component of the thrust vector to apply in the Velocity direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
W_NormalDirection
|
The component of the thrust vector to apply in the Orbit Normal direction
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
X_Component
|
For AttitudeSystem = 0, ICRF X-directed component of the maneuver.
For AttitudeSystem = 1, Velocity directed component of the maneuver.
For AttitudeSystem = 2, Co-Velocity directed component of the maneuver.
For AttitudeSystem = 3, Body coordinate X-directed component of the maneuver.
For AttitudeSystem = 4, Y cross Z directed component of the maneuver.
For AttitudeSystem = 5, Position directed component of the maneuver.
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
Y_Component
|
For AttitudeSystem = 0, ICRF Y-directed component of the maneuver.
For AttitudeSystem = 1, Orbit Normal directed component of the maneuver.
For AttitudeSystem = 2, Negative Orbit Normal directed component of the maneuver.
For AttitudeSystem = 3, Body coordinate Y-directed component of the maneuver.
For AttitudeSystem = 4, Negative Orbit Normal directed component of the maneuver.
For AttitudeSystem = 5, Velocity directed component of the maneuver.
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|
Z_Component
|
For AttitudeSystem = 0, ICRF Z-directed component of the maneuver.
For AttitudeSystem = 1, Orbit Bi-Normal directed component of the maneuver.
For AttitudeSystem = 2, Nadir directed component of the maneuver.
For AttitudeSystem = 3, Body coordinate Z-directed component of the maneuver.
For AttitudeSystem = 4, Intersection Normal to the Earth's Surface directed component of the maneuver.
For AttitudeSystem = 5, Orbit Normal directed component of the maneuver.
This property has been Deprecated. Please use BurnDirection instead.
|
Type: Variable
Access: Read/Write
Units: km/s^2
|