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ACS Ctrl Bug Bash #439

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muellerr merged 42 commits from acs-bug-bash into develop 2023-03-10 19:21:19 +01:00
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1 changed files with 6 additions and 6 deletions
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12
mission/controller/acs/AcsParameters.h
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@ -783,9 +783,9 @@ class AcsParameters : public HasParametersIF {
struct RwHandlingParameters { struct RwHandlingParameters {
double inertiaWheel = 0.000028198; double inertiaWheel = 0.000028198;
double maxTrq = 0.0032; // 3.2 [mNm] double maxTrq = 0.0032; // 3.2 [mNm]
int32_t stictionSpeed = 100; // RPM int32_t stictionSpeed = 100; // RPM
int32_t stictionReleaseSpeed = 120; // RPM int32_t stictionReleaseSpeed = 120; // RPM
double stictionTorque = 0.0006; double stictionTorque = 0.0006;
uint16_t rampTime = 10; uint16_t rampTime = 10;
@ -843,7 +843,7 @@ class AcsParameters : public HasParametersIF {
double refDirection[3] = {-1, 0, 0}; // Antenna double refDirection[3] = {-1, 0, 0}; // Antenna
double refRotRate[3] = {0, 0, 0}; double refRotRate[3] = {0, 0, 0};
double quatRef[4] = {0, 0, 0, 1}; double quatRef[4] = {0, 0, 0, 1};
int8_t timeElapsedMax = 10; // rot rate calculations uint8_t timeElapsedMax = 10; // rot rate calculations
// Default is Stuttgart GS // Default is Stuttgart GS
double latitudeTgt = 48.7495 * M_PI / 180.; // [rad] Latitude double latitudeTgt = 48.7495 * M_PI / 180.; // [rad] Latitude
@ -859,7 +859,7 @@ class AcsParameters : public HasParametersIF {
struct GsTargetModeControllerParameters : PointingLawParameters { struct GsTargetModeControllerParameters : PointingLawParameters {
double refDirection[3] = {-1, 0, 0}; // Antenna double refDirection[3] = {-1, 0, 0}; // Antenna
int8_t timeElapsedMax = 10; // rot rate calculations uint8_t timeElapsedMax = 10; // rot rate calculations
// Default is Stuttgart GS // Default is Stuttgart GS
double latitudeTgt = 48.7495 * M_PI / 180.; // [rad] Latitude double latitudeTgt = 48.7495 * M_PI / 180.; // [rad] Latitude
@ -871,7 +871,7 @@ class AcsParameters : public HasParametersIF {
double refDirection[3] = {-1, 0, 0}; // Antenna double refDirection[3] = {-1, 0, 0}; // Antenna
double quatRef[4] = {0, 0, 0, 1}; double quatRef[4] = {0, 0, 0, 1};
double refRotRate[3] = {0, 0, 0}; double refRotRate[3] = {0, 0, 0};
int8_t timeElapsedMax = 10; // rot rate calculations uint8_t timeElapsedMax = 10; // rot rate calculations
} nadirModeControllerParameters; } nadirModeControllerParameters;
struct InertialModeControllerParameters : PointingLawParameters { struct InertialModeControllerParameters : PointingLawParameters {