3 new parameters in src/.
- Added 3 parameters:
MC_REF_FF=0.0,MC_REF_FF_MAX=100.0andMC_REF_W_N=50.0. - Most activity in
src/(+37/−0).
Full analysis → Summary: automatic analysis
MC_REF_FF = 0.0, MC_REF_FF_MAX = 100.0 and MC_REF_W_N = 50.0.src/ (+37/−0).Full analysis → Summary: automatic analysis
None.
| Name | Value | Type | File |
|---|---|---|---|
MC_REF_FF | 0.0 | number | src/modules/mc_att_control/mc_att_control_params.yaml |
MC_REF_FF_MAX | 100.0 | number | src/modules/mc_att_control/mc_att_control_params.yaml |
MC_REF_W_N | 50.0 | number | src/modules/mc_att_control/mc_att_control_params.yaml |
230/280 weighted chars
| Module | Added | Modified | Removed | Lines + | Lines − |
|---|---|---|---|---|---|
src | 0 | 1 | 0 | +37 | −0 |
| Path | Lines | Note | |
|---|---|---|---|
| M | src/modules/mc_att_control/mc_att_control_params.yaml | +37/−0 |
feat(mc_att_control): feedforward filtered q_d derivative on rate sp (#27255) Add a 2nd-order critically-damped attitude reference model whose angular-velocity output is fed forward onto the rate setpoint, removing the steady-state ramp-tracking lag of the pure-P attitude law. The model uses an exact closed-form discretisation, so it is unconditionally stable. Parameters: - MC_REF_W_N reference-model bandwidth [rad/s] - MC_REF_FF feedforward gain [0..1]; 0 disables the anticipation - MC_REF_FF_MAX per-axis feedforward saturation [deg/s] The commanded yaw rate is always fed forward at unity (it is a setpoint, not a model prediction), so MC_REF_FF scales only the error-driven anticipation and MC_REF_FF=0 is the exact legacy pure-P law. Shipped disabled by default to avoid changing behaviour on existing platforms; enable per-airframe. Includes docs and the updated controller diagram.