A representation of a rocket thruster on the robot More...
Public Member Functions | |
void | GetThrusterFacingDirection (out double x, out double y, out double z) |
Returns a unit vector representing the direction that this thruster pushes the robot when the current speed is more than zero. This unit vector is relative to the robot, not the world. More... | |
void | GetOffsetFromRobotCenterOfMass (out double x, out double y, out double z) |
Returns the offset from the end of this thruster to the robot's center of mass, in meters. This vector is relative to the robot, not the world. More... | |
Properties | |
IRobotExplorer | Robot [get] |
The robot this thruster is attached to More... | |
int | PropellerIndex [get] |
The index of this thruster in the robot's list of propellers More... | |
double | MaxThrust [get] |
Maximum amount of force applied by the thruster More... | |
double | CurrentThrustAmount [get] |
The target amount of thrust applied, from zero (closed nozzle) to one (open nozzle) More... | |
double | TargetThrustAmount [get, set] |
The target amount of thrust applied, from zero (closed nozzle) to one (open nozzle) More... | |
A representation of a rocket thruster on the robot
void IRobotThruster.GetOffsetFromRobotCenterOfMass | ( | out double | x, |
out double | y, | ||
out double | z | ||
) |
Returns the offset from the end of this thruster to the robot's center of mass, in meters.
This vector is relative to the robot, not the world.
void IRobotThruster.GetThrusterFacingDirection | ( | out double | x, |
out double | y, | ||
out double | z | ||
) |
Returns a unit vector representing the direction that this thruster pushes the robot when the current speed is more than zero. This unit vector is relative to the robot, not the world.
|
get |
The target amount of thrust applied, from zero (closed nozzle) to one (open nozzle)
|
get |
Maximum amount of force applied by the thruster
|
get |
The index of this thruster in the robot's list of propellers
|
get |
The robot this thruster is attached to
|
getset |
The target amount of thrust applied, from zero (closed nozzle) to one (open nozzle)