stabilization_heli_indi

INDI stabilization controller for helicopters

Section RC_SETPOINT

STABILIZATION_ATTITUDE_

Name

Value

Description

SP_MAX_PHI

45.

max setpoint for roll angle

SP_MAX_THETA

45.

max setpoint for pitch angle

SP_MAX_R

90.

max setpoint for yaw rate

DEADBAND_R

250

deadband on yaw rate input

Section ATTITUDE_REFERENCE

STABILIZATION_ATTITUDE_

Name

Value

Description

REF_OMEGA_P

400

reference generator omega param on roll rate

REF_ZETA_P

0.9

reference generator zeta param on roll rate

REF_MAX_P

300.

reference generator max roll rate

REF_MAX_PDOT

RadOfDeg(7000.)

reference generator max roll acceleration

REF_OMEGA_Q

400

reference generator omega param on pitch rate

REF_ZETA_Q

0.9

reference generator zeta param on pitch rate

REF_MAX_Q

300.

reference generator max pitch rate

REF_MAX_QDOT

RadOfDeg(7000.)

reference generator max pitch acceleration

REF_OMEGA_R

250

reference generator omega param on yaw rate

REF_ZETA_R

0.9

reference generator zeta param on yaw rate

REF_MAX_R

180.

reference generator max yaw rate

REF_MAX_RDOT

RadOfDeg(1800.)

reference generator max yaw acceleration

Section STABILIZATION_ATTITUDE_INDI

STABILIZATION_INDI_

Name

Value

Description

G1_P

0.0639

control effectiveness G1 gain on roll rate

G1_Q

0.0361

control effectiveness G1 gain on pitch rate

G1_R

0.0022

control effectiveness G1 gain on yaw rate

G2_R

0.1450

control effectiveness G2 gain on yaw rate

REF_ERR_P

600.0

reference acceleration

REF_ERR_Q

600.0

reference acceleration

REF_ERR_R

600.0

reference acceleration

REF_RATE_P

28.0

reference acceleration

REF_RATE_Q

28.0

reference acceleration

REF_RATE_R

28.0

reference acceleration

MAX_R

120.0

max yaw rate

FILT_CUTOFF

8.0

second order cutoff parameter

ESTIMATION_FILT_CUTOFF

8.0

second order cutoff parameter

ACT_DYN_P

0.1

first order actuator dynamics on roll rate

ACT_DYN_Q

0.1

first order actuator dynamics on pitch rate

ACT_DYN_R

0.1

first order actuator dynamics on yaw rate

USE_ADAPTIVE

FALSE|TRUE

enable adaptive gains

ADAPTIVE_MU

0.0001

adaptation parameter

Depends

  • stabilization_rotorcraft
  • @attitude_command

Provides

  • commands

Sections