[FS2004] - Wilco + Fifty North Merge v2.1 - Boeing 733/734/735 (Aircraft)

[Autopilot]
; Pitch limits
; noseup
maxPitch=25.0
; nosedown
minPitch=-15.0
;Bank
bankStep=3.0
; Pitch hold
; Proportional component. Target pitchrate is pitch_spd_Kp * (target_pitch - current_pitch)
pitch_spd_Kp=2.0
; Integral component
pitch_spd_Ki=0.0
; min/max rollrate
pitch_spd_min_output=-2.5
pitch_spd_max_output=2.5
; 2nd stage PID controller
pitch_gain_lo_alt_breakpoint=15000
pitch_gain_hi_alt_breakpoint=35000
; gain at lower and higher altitudes. At average altitudes gain will be interpolated
pitch_lo_alt_Kp=-0.10
pitch_hi_alt_Kp=-0.04
; Integrator time (seconds)
pitch_Ti=1.0
; Derivator time (seconds)
pitch_Td=0.125
; Bank limit
maxBank=28.0
halfBank=17.0
; Bank hold
; Proportional component. Target rollrate is bank_spd_Kp * (target_bank - current_bank)
bank_spd_Kp=0.4
; Integral component
bank_spd_Ki=0.0
; min/max rollrate
bank_spd_min_output=-2.5
bank_spd_max_output=2.5
; 2nd stage PID controller
bank_gain_lo_alt_breakpoint=10000
bank_gain_hi_alt_breakpoint=35000
; gain at lower and higher altitudes. At average altitudes gain will be interpolated
bank_lo_alt_Kp=-0.040
bank_hi_alt_Kp=-0.020
; Integrator time (seconds)
bank_Ti=1.0
; Derivator time (seconds)
bank_Td=0.001
;AP will apply more aileron to level wings
turnBackForceScalar=1.3
; scalar will applied when target bank < bfThreshold * currentBank
bfThreshold=0.8
;Hold and turns processing
trate_Kp=0.01
trate_Ti=0.1
trate_Td=0.005
trate_min_output=-10
trate_max_output=10
; additional rate when off track
ttarget_Kp=-0.5
ttarget_Ki=0
;Perform automatic elevator trimming when autopilot is active
autotrim=1
; Low speed autotrim rate per second (flaps retracted)
trim_lo_rate=0.02
; High speed autotrim rate per second (flaps extended)
trim_hi_rate=0.03
; If average elevator position less than specified position trim will not move
trim_elev_threshold=0.02
; If non zero pilot can overforce AP with yoke to drop into CWS mode or even disconnect AP
enableApOverforce=0
; If yoke beyond this position, CWS P mode engages
cwsp_on=0.500000
; If yoke below this position, CWS P mode disengages (AP holds pitch)
cwsp_off=0.200000
; If yoke beyond this position, AP will disengages
cwsp_ap_off=0.900000
; If yoke beyond this position, CWS R mode engages
cwsr_on=0.500000
; If yoke below this position, CWS R mode disengages (AP holds bank or heading)
cwsr_off=0.200000
; If yoke beyond this position, AP will disengages
cwsr_ap_off=0.900000
; Vertical speed hold
; Proportional component. Target vsrate is vs_spd_Kp * (target_vs - current_vs)
vs_spd_Kp=2.0
; Integral component
vs_spd_Ki=0.0
; min/max vsrate
vs_spd_min_output=-1500
vs_spd_max_output=1500
; 2nd stage PID controller
vs_gain_lo_alt_breakpoint=15000
vs_gain_hi_alt_breakpoint=35000
; gain at lower and higher altitudes. At average altitudes gain will be interpolated
vs_lo_alt_Kp=-0.0000004
vs_hi_alt_Kp=-0.0000003
//vs_Kp=-0.0000003
; Integrator time (seconds)
vs_Ti=0.00125
; Derivator time (seconds)
vs_Td=0.002
;Max difference between current and target value (cropping if actual difference is bigger)
vs_max_diff=1000
; Vertical speed prediction time (seconds)
vs_fpm_prediction_time=1.0
; prediction filter gain
vs_fpm_prediction_filter=0.8
; Altitude hold P [ + I ] controller
; Proportional component. Target cimbrate is alt_Kp * (target_alt - current_alt)
alt_Kp=1.7
; Integral component
alt_Ki=0.0
; min/max climbrate in altitude hold
alt_min_output=-500
alt_max_output=500
; LVL CHG
; target acceleration P [ + I ] controller
; Proportional component. Target acceleration is lvlchg_acc_Kp * (target_speed - current_speed)
lvlchg_acc_Kp=0.5
; Integral component
lvlchg_acc_Ki=0.0
; min/max acceleration in LVL CHG
; acceleration measured in knots per lvlchg_cas_prediction_time seconds
lvlchg_acc_min_output=-5
lvlchg_acc_max_output=5
; LVL CHG PID controller
lvlchg_Kp=0.000015
; Integrator time (seconds)
lvlchg_Ti=0.0005
; Derivator time (seconds)
lvlchg_Td=0.001
; Speed prediction time (seconds)
lvlchg_cas_prediction_time=5.0
; Speed prediction filter gain
lvlchg_cas_prediction_filter=0.1
; Difference between target and current predicted speed (lvlchg_cas_prediction_time seconds ahead)
; when pitching to hold target speed is enabled
lvlchg_capture_cas_diff=5
; Difference between target and current predicted speed (lvlchg_cas_prediction_time seconds ahead)
; when pitching to hold target speed is disabled
lvlchg_loose_cas_diff=20
lvlchg_climb_accelerate_fpm=1000
lvlchg_descent_decelerate_fpm=-500
; LVL CHG by default AP
defIasKp=40
defIasKd=5
; Altitude intercept P [ + I ] controller
; Proportional component. Target cimbrate is alt_Kp * (target_alt - current_alt)
altacq_Kp=4.0
; Integral component
altacq_Ki=0.0
; min/max climbrate in ALT ACQ
altacq_min_output=-2500
altacq_max_output=2500
altacq_lo_alt_breakpoint=10000
altacq_hi_alt_breakpoint=35000
; Point when ALT ACQ mode will engaged at lower and higher altitudes. At average altitudes gain will be interpolated
; For ex. when value is 0.2 and climb rate is 3000 fpm, ALT ACQ will engaged at 3000 * 0.2 = 600 feet before target altitude
altacq_lo_alt_K=0.20
altacq_hi_alt_K=0.20
; GS hold P [ + I ] controller
; Proportional component
gs_Kp=-5.0
; Integral component
gs_Ki=0.0
gs_min_output=-300
gs_max_output=300
; VNAV descent path hold P [ + I ] controller
; Proportional component
vnav_Kp=-20.0
; Integral component
vnav_Ki=0.0
vnav_min_output=-2000
vnav_max_output=2000
; for CI = 0
vnavMinPathAngle=3.25
; for CI = 200
vnavMaxPathAngle=3.75
; trim percentage on final to add
; trim added on 400 feet
trim_400=0.02
; trim added on 50 feet
trim_50=0.02
; HDG SEL P [ + I ] controller
; Proportional component. Target bank is hdg_Kp * (target_hdg - current_hdg)
; hdg_Kp is depends from ground speed now
hdg_LoSpd=250
hdg_HiSpd=400
hdg_LoKp=-0.8
hdg_HiKp=-1.6
; Integral component
hdg_Ki=0.0
; VOR hold P [ + I ] controller
; Proportional component
vor_Kp=10
; Integral component
vor_Ki=0.0
vor_min_output=-20
vor_max_output=20
; VAPP hold P [ + I ] controller
; Proportional component
vapp_Kp=20
; Integral component
vapp_Ki=0.0
vapp_min_output=-40
vapp_max_output=40
; LOC/BC hold P [ + I ] controller
; Proportional component
loc_Kp=7.5
; Integral component
loc_Ki=0.0
loc_min_output=-30
loc_max_output=30
;LNAV mode
lnav_Kp=30
lnav_Ki=0
lnav_min_output=-30
lnav_max_output=30
;max bank in LNAV turns
lnav_max_bank=23
;when IAS below
lnav_max_bank_ias = 220
Заменить до этой секции!!!!!!!!!!!!!!!!!
; THR HOLD mode
; if nonzero, not allows free throttle movement
holdThrottles=0