sunSafePoint#
Executive Summary#
This module provides the attitude guidance output for a sun pointing mode. This could be used for safe mode, or a power generation mode. The input is the sun direction vector which does not have to be normalized, as well as the body rate information. The output is the standard BSK attitude reference state message. The sun direction measurement is cross with the desired body axis that is to point at the sun to create a principle rotation vector. The dot product between these two vectors is used to extract the principal rotation angle. With these a tracking error MRP state is computer. The body rate tracking errors relative to the reference frame are set equal to the measured body rates to bring the vehicle to rest when pointing at the sun. Thus, the reference angular rate and acceleration vectors relative to the inertial frame are nominally set to zero. If the sun vector is not available, then the reference rate is set to a body-fixed value while the attitude tracking error is set to zero.
The file
PDF Description.
contains further information on this module’s function, how to run it, as well as testing.
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 |
|---|---|---|
attGuidanceOutMsg |
AttGuidMsgPayload |
attitude guidance output message |
sunDirectionInMsg |
NavAttMsgPayload |
sun direction input message |
imuInMsg |
NavAttMsgPayload |
IMU input message |
Class SunSafePoint#
-
class SunSafePoint : public SysModel#
Top level structure for the sun-safe attitude guidance routine.
Public Functions
-
void reset(uint64_t callTime) override#
This method performs a complete reset of the module. Local module variables that retain time varying states between function calls are reset to their default values.
- 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
Public Members
-
Message<AttGuidMsgPayload> attGuidanceOutMsg#
The name of the output message
-
ReadFunctor<NavAttMsgPayload> sunDirectionInMsg#
The name of the Input message
-
ReadFunctor<NavAttMsgPayload> imuInMsg#
The name of the incoming IMU message
-
double minUnitMag#
— The minimally acceptable norm of sun body vector
-
double sunAngleErr#
rad The current error between cmd and obs sun angle
-
double smallAngle#
rad An angle value that specifies what is near 0 or 180 degrees
-
double eHat180_B[3]#
— Eigen axis to use if commanded axis is 180 from sun axis
-
double sunMnvrVec[3]#
— The eigen axis that we want to rotate on to get sun
-
double sHatBdyCmd[3]#
— Desired body vector to point at the sun
-
double omega_RN_B[3]#
— Desired body rate vector if no sun direction is available
-
double sunAxisSpinRate#
r/s Desired constant spin rate about sun heading vector
-
AttGuidMsgPayload attGuidanceOutBuffer#
— The output data that we compute
-
BSKLogger bskLogger = {}#
BSK Logging.
-
void reset(uint64_t callTime) override#