Gautier Hattenberger d58602b7bb [settings] ROLL_MAX_SETPOINT with correct step (float) and unit

2015-01-19 16:17:41 +01:00

..

ctl_adaptive_h_ff.xml

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ctl_adaptive.xml

[settings] ROLL_MAX_SETPOINT with correct step (float) and unit

2015-01-19 16:17:41 +01:00

ctl_basic.xml

[settings] ROLL_MAX_SETPOINT with correct step (float) and unit

2015-01-19 16:17:41 +01:00

ctl_dash_loiter_trim.xml

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ctl_energy.xml

[settings] ROLL_MAX_SETPOINT with correct step (float) and unit

2015-01-19 16:17:41 +01:00

ctl_energyadaptive.xml

[settings] ROLL_MAX_SETPOINT with correct step (float) and unit

2015-01-19 16:17:41 +01:00

ctl_new_airspeed.xml

[settings] ROLL_MAX_SETPOINT with correct step (float) and unit

2015-01-19 16:17:41 +01:00

ctl_new.xml

[settings] ROLL_MAX_SETPOINT with correct step (float) and unit

2015-01-19 16:17:41 +01:00

ctl_rate.xml

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rotorcraft_guidance.xml

[rotorcraft] horizontal guidance reference refactor

2014-08-28 18:50:39 +02:00

stabilization_att_float_euler.xml

[stabilization] float_euler fixes so it actually compiles

2013-10-23 11:39:14 +02:00

stabilization_att_float_quat.xml

[conf] settings: fix typos in stabilization_att_float_quat

2014-04-06 23:21:27 +02:00

stabilization_att_int_quat.xml

[ahrs] quaternion integrator fix

2014-10-28 18:57:11 +01:00

stabilization_att_int.xml

[ahrs] quaternion integrator fix

2014-10-28 18:57:11 +01:00

stabilization_rate.xml

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tune_agr_climb.xml

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