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chore(X500): update the template #1024
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| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -1,13 +1,13 @@ | ||
| ATC_ANG_PIT_P,4.5 | ||
| ATC_ANG_RLL_P,4.5 | ||
| ATC_ANG_YAW_P,4.5 | ||
| ATC_INPUT_TC,0.15 | ||
| ATC_RAT_PIT_D,0.0036 # = 1* (0.0036 default) | ||
| ATC_RAT_PIT_I,0.121 # = 0.896 * (0.135 default) | ||
| ATC_RAT_PIT_P,0.121 # = 0.896 * (0.135 default) | ||
| ATC_RAT_RLL_D,0.0036 # = 1 * (0.0036 default) | ||
| ATC_RAT_RLL_I,0.121 # = 0.896 * (0.135 default) | ||
| ATC_RAT_RLL_P,0.121 # = 0.896 * (0.135 default) | ||
| ATC_INPUT_TC,0.2 # It's a small (too fast) copter | ||
| ATC_RAT_PIT_D,0.00432 # = 1.2* (0.0036 default) | ||
| ATC_RAT_PIT_I,0.162 # = 1.2 * (0.135 default) | ||
| ATC_RAT_PIT_P,0.162 # = 1.2 * (0.135 default) | ||
| ATC_RAT_RLL_D,0.00432 # = 1.2* (0.0036 default) | ||
| ATC_RAT_RLL_I,0.162 # = 1.2 * (0.135 default) | ||
| ATC_RAT_RLL_P,0.162 # = 1.2 * (0.135 default) | ||
| ATC_RAT_YAW_D,0 # = 1 * (0 default) | ||
| ATC_RAT_YAW_I,0.018 # = 1 * (0.018 default) | ||
| ATC_RAT_YAW_P,0.18 # = 1 * (0.18 default) | ||
| ATC_RAT_YAW_I,0.026 # = 1.2 * (0.018 default) | ||
| ATC_RAT_YAW_P,0.26 # = 1.2 * (0.18 default) | ||
| Original file line number | Diff line number | Diff line change | ||||
|---|---|---|---|---|---|---|
| @@ -0,0 +1,23 @@ | ||||||
| ANGLE_MAX,3000 # limit the angle to limit the speed at SID-chirp low-frequencies | ||||||
| ARMING_CHECK,30174 # disable Parameter check because we need to set ATC_RAT_RLL_I out-of-range (was 1) | ||||||
| ATC_ANG_PIT_P,24.629694 | ||||||
| ATC_ANG_RLL_P,18.379057 | ||||||
| ATC_ANG_YAW_P,7.636879 | ||||||
| ATC_RAT_PIT_I,0.180513 | ||||||
| ATC_RAT_RLL_I,0.155054 | ||||||
| ATC_RAT_YAW_I,0.099616 | ||||||
| ATC_RATE_FF_ENAB,1 # normal operation | ||||||
| FLTMODE6,25 # Activate sysid instead of loiter | ||||||
| LOG_BITMASK,145119 # attitude sample rate at 400Hz rate | ||||||
| LOG_DISARMED,0 # was only needed for wind speed estimation | ||||||
| LOG_REPLAY,0 # was only needed for wind speed estimation | ||||||
| SID_AXIS,1 # Inject chip on the input roll signal | ||||||
|
||||||
| SID_AXIS,1 # Inject chip on the input roll signal | |
| SID_AXIS,1 # Inject chirp on the input roll signal |
| Original file line number | Diff line number | Diff line change | ||||
|---|---|---|---|---|---|---|
| @@ -0,0 +1,23 @@ | ||||||
| ANGLE_MAX,3000 # limit the angle to limit the speed at SID-chirp low-frequencies | ||||||
| ARMING_CHECK,30174 # disable Parameter check because we need to set ATC_RAT_RLL_I out-of-range (was 1) | ||||||
| ATC_ANG_PIT_P,24.629694 | ||||||
| ATC_ANG_RLL_P,18.379057 | ||||||
| ATC_ANG_YAW_P,7.636879 | ||||||
| ATC_RAT_PIT_I,0.180513 | ||||||
| ATC_RAT_RLL_I,0.155054 | ||||||
| ATC_RAT_YAW_I,0.099616 | ||||||
| ATC_RATE_FF_ENAB,1 # normal operation | ||||||
| FLTMODE6,25 # Activate sysid instead of loiter | ||||||
| LOG_BITMASK,145119 # attitude sample rate at 400Hz rate | ||||||
| LOG_DISARMED,0 # was only needed for wind speed estimation | ||||||
| LOG_REPLAY,0 # was only needed for wind speed estimation | ||||||
| SID_AXIS,2 # Inject chip on the input pitch signal | ||||||
|
||||||
| SID_AXIS,2 # Inject chip on the input pitch signal | |
| SID_AXIS,2 # Inject chirp on the input pitch signal |
| Original file line number | Diff line number | Diff line change | ||||
|---|---|---|---|---|---|---|
| @@ -0,0 +1,23 @@ | ||||||
| ANGLE_MAX,3000 # limit the angle to limit the speed at SID-chirp low-frequencies | ||||||
| ARMING_CHECK,30174 # disable Parameter check because we need to set ATC_RAT_RLL_I out-of-range (was 1) | ||||||
| ATC_ANG_PIT_P,24.629694 | ||||||
| ATC_ANG_RLL_P,18.379057 | ||||||
| ATC_ANG_YAW_P,7.636879 | ||||||
| ATC_RAT_PIT_I,0.180513 | ||||||
| ATC_RAT_RLL_I,0.155054 | ||||||
| ATC_RAT_YAW_I,0.099616 | ||||||
| ATC_RATE_FF_ENAB,1 # normal operation | ||||||
| FLTMODE6,25 # Activate sysid instead of loiter | ||||||
| LOG_BITMASK,145119 # attitude sample rate at 400Hz rate | ||||||
| LOG_DISARMED,0 # was only needed for wind speed estimation | ||||||
| LOG_REPLAY,0 # was only needed for wind speed estimation | ||||||
| SID_AXIS,3 # Inject chip on the input yaw signal | ||||||
|
||||||
| SID_AXIS,3 # Inject chip on the input yaw signal | |
| SID_AXIS,3 # Inject chirp on the input yaw signal |
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[nitpick] The comment 'It's a small (too fast) copter' is unclear. Consider revising to explain why a larger time constant (0.2 vs 0.15) is appropriate, e.g., 'Increased time constant for smoother control response on this small, agile copter'.