dvAttEffect#
Executive Summary#
This module implements a DV attitude effector management algorithm. This algorithm is used to control both the RCS and DV thrusters when executing a trajectory adjustment.
Message Connection Descriptions#
The following table lists all the module input and output messages. The module msg connection is set by the user from python. The msg type contains a link to the message structure definition, while the description provides information on what this message is used for.
Msg Variable Name |
Msg Type |
Description |
---|---|---|
cmdTorqueBodyInMsg |
CmdTorqueBodyMsgPayload |
attitude reference output message |
thrOnTimeOutMsg |
THRArrayOnTimeCmdMsgPayload |
thruster on-time output message for each thruster group |
Class DvAttEffect#
-
class DvAttEffect : public SysModel#
module configuration message
Public Functions
-
void reset(uint64_t callTime) override#
This method resets the module.
- Parameters:
callTime – The clock time at which the function was called (nanoseconds)
- Returns:
void
-
void updateState(uint64_t callTime) override#
This method takes the estimated body-observed sun vector and computes the current attitude/attitude rate errors to pass on to control.
- Parameters:
callTime – The clock time at which the function was called (nanoseconds)
- Returns:
void
-
void reset(uint64_t callTime) override#