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Thread: FS2004 Canard Control Question

  1. #1

    Question FS2004 Canard Control Question

    I am in the midst of modelling a Rutan Vari-Viggan in Gmax and have come up with a bit of a problem. As some of you may know, the Vari-Viggan used a flap like "elevator" surface that functioned to either increase the lift on the canard (as in "up elevator") or decrease the lift (down elevator). I have tried googeling the issue and have met with little success. The only two articles that matched my search both stated to "reverse the pivot axis'". I tried that and, while the physical movement of the "elevator" matched the stick input, the reaction was exactly reverse of what was expected (ie - pulling back on the stick causes a nose down pitch and pushing forward on the stick causes a nose up pitch.) Reversing the elevator input in the "Control" section of the "Options" page has no effect. Please advise.

  2. Default

    I am very familiar with that design. It's one that has been on my "short list" of planes to make. I'm afraid your description is confusing to me, so I'll start with a basic description of what it should look like and we'll go from there. When you pull back on the stick the "elevators" should pivot down, and the plane should climb. I would not adjust any controller settings as that will possibly mess up all your other planes. I think there is something in the aircraft.cfg file that controls this. I will need to do some research for you, but you need to be a bit patient as I am currently recovering my system after being hit by a virus.

  3. #3

    Default

    Thanks for your response! That's exactly what I was talking about. I shall await the results of your research. Bye the way, sorry to hear of your infection. I sincerely hope nothing of importance was lost.

  4. #4

    Default

    N2056, have you had a chance to look into the problem I'm having yet?

  5. #5

    Default

    You may need to reverse the sign of the elevator derivatives in the .air file

  6. Default

    Could you post your aircraft.cfg so we can look it over?

  7. #7

    Default

    Sure thing. Here it is:

    [fltsim.0]
    title=VV01test
    sim=SingleEngineProp
    model=
    panel=
    panel_alias = c172\panel
    sound=
    sound_alias = c172\sound
    texture=
    kb_checklists=
    kb_reference=
    atc_id=N27VV
    ui_manufacturer=Rutan Aircraft Factory
    ui_type=SingleEngineProp
    ui_variation=Model 27
    description=ADD NEW DESCRIPTION HERE While a number of enhancements make it a step forward in development, the 182S retains the remarkable characteristics that have made the 182 a popular airplane: power, stability, and good load hauling capabilities. The Skylane 182S is an ideal airplane for pilot training. If you're new to flying, you'll find Rod Machado's flight lessons in the 182S very helpful. You'll find them in the Flight Simulator 2000 Pilot's Handbook. For enhanced instrument flight rules (IFR) panels, choose the 182S IFR. See the Aircraft Information section of Help for tips on flying this aircraft.
    atc_heavy=0
    atc_airline=
    atc_flight_number=

    [General]
    atc_type=Rutan
    atc_model=27
    performance=General characteristics:\n\tCrew: 2\n\tLength: 16 ft 10 in\n\tWingspan: 19 ft 0 in\n\tWing area: 123 ft²\n\tEmpty weight: 1020 lb\n\tMax. takeoff weight: 1700 lb\n\nPerformance:\n\tMaximum speed: 165 mph\n\tCruise speed: 150 mph \n\tStall speed: 48 mph\n\tRange: 400 mi\n\tRate of climb: 800 ft\/min\n

    [WEIGHT_AND_BALANCE]
    max_gross_weight = 1700.000
    empty_weight = 1020.000

    reference_datum_position = 0.000, 0.000, 0.000
    empty_weight_CG_position = 0.000, 0.000, 0.000

    max_number_of_stations = 50

    station_load.0 =170.000000, -4.500000, 0.000000, 0.000000, longitudinal
    station_load.1 =170.000000, -1.000000, 0.000000, 0.000000, longitudinal
    station_load.2 =0.000000, 0.000000, 0.000000, 0.000000, longitudinal
    station_load.3 = 0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
    station_load.4 = 0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

    ;Moments of Inertia
    empty_weight_pitch_MOI = 1400.000
    empty_weight_roll_MOI = 1137.000
    empty_weight_yaw_MOI = 2360.000
    empty_weight_coupled_MOI= 0.000
    CG_forward_limit= 0.000
    CG_aft_limit= 1.000


    [flight_tuning]
    cruise_lift_scalar =1.000
    parasite_drag_scalar =0.930
    induced_drag_scalar =1.000
    elevator_effectiveness =1.202
    aileron_effectiveness =1.000
    rudder_effectiveness =1.000
    pitch_stability =1.000
    roll_stability =1.000
    yaw_stability =1.000
    elevator_trim_effectiveness =1.000
    aileron_trim_effectiveness =1.000
    rudder_trim_effectiveness =1.000

    [GeneralEngineData]
    engine_type = 0
    Engine.0 = -3.510, 0.000, 0.693
    fuel_flow_scalar= 0.880
    min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser

    [piston_engine]
    power_scalar =1.000
    cylinder_displacement= 80.000
    compression_ratio= 8.500
    number_of_cylinders= 4
    max_rated_rpm= 2700.000
    max_rated_hp= 160.000
    fuel_metering_type= 0
    cooling_type= 0
    normalized_starter_torque= 0.300
    turbocharged= 0
    max_design_mp= 0.000
    min_design_mp= 0.000
    critical_altitude= 0.000
    emergency_boost_type= 0
    emergency_boost_mp_offset= 0.000
    emergency_boost_gain_offset= 0.000
    fuel_air_auto_mixture= 0
    auto_ignition= 0
    max_rpm_mechanical_efficiency_scalar=1.000
    idle_rpm_mechanical_efficiency_scalar=1.000
    max_rpm_friction_scalar=1.000
    idle_rpm_friction_scalar=1.000

    [propeller]
    thrust_scalar =1.000
    propeller_type= 1
    propeller_diameter= 4.930
    propeller_blades= 3
    propeller_moi= 3.000
    beta_max= 0.000
    beta_min= 0.000
    min_gov_rpm= 0.000
    prop_tc= 0.000
    gear_reduction_ratio= 1.000
    fixed_pitch_beta= 20.000
    low_speed_theory_limit= 80.000
    prop_sync_available= 0
    prop_deice_available= 0
    prop_feathering_available= 0
    prop_auto_feathering_available= 0
    min_rpm_for_feather= 0.000
    beta_feather= 0.000
    power_absorbed_cf= 0.000
    defeathering_accumulators_available= 0
    prop_reverse_available= 0.000
    minimum_on_ground_beta= 0.000
    minimum_reverse_beta= 0.000

    [electrical]
    ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
    flap_motor = 0, 5 , 17.0
    gear_motor = 0, 5 , 17.0
    autopilot = 0, 5 , 17.0
    avionics_bus = 0, 5 , 17.0
    avionics = 1, 5 , 17.0
    pitot_heat = 0, 2 , 17.0
    additional_system = 0, 2 , 17.0
    marker_beacon = 1, 2 , 17.0
    gear_warning = 0, 2 , 17.0
    fuel_pump = 0, 5 , 17.0
    starter1 = 0, 20, 17.0
    light_nav = 0, 5 , 17.0
    light_beacon = 0, 5 , 17.0
    light_landing = 0, 5 , 17.0
    light_taxi = 0, 5 , 17.0
    light_strobe = 0, 5 , 17.0
    light_panel = 0, 5 , 17.0

    //0 Class
    //1 Longitudinal Position (feet)
    //2 Lateral Position (feet)
    //3 Vertical Position (feet)
    //4 Impact Damage Threshold (Feet Per Minute)
    //5 Brake Map (0=None, 1=Left, 2=Right)
    //6 Wheel Radius (feet)
    //7 Steer Angle (degrees)
    //8 Static Compression (feet) (0 if rigid)
    //9 Max/Static Compression Ratio
    //10 Damping Ratio (0=Undamped, 1=Critically Damped)
    //11 Extension Time (seconds)
    //12 Retraction Time (seconds)
    //13 Sound Type
    [contact_points]
    point.0 = 1.000, 7.287, 0.000, -3.370, 1500.000, 0.000, 0.375, 22.000, 0.210, 1.636, 0.500, 6.000, 6.000, 0.000, 0.000, 0.000
    point.1 = 1.000, -2.070, -3.057, -3.370, 3500.000, 1.000, 0.554, 0.000, 0.217, 1.931, 0.500, 6.000, 6.000, 2.000, 0.000, 0.000
    point.2 = 1.000, -2.070, 3.057, -3.370, 3500.000, 2.000, 0.500, 0.000, 0.217, 1.931, 0.500, 6.000, 6.000, 3.000, 0.000, 0.000
    point.3 = 2.000, -0.400, -9.450, -1.225, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
    point.4 = 2.000, -0.400, 9.450, -1.225, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
    point.5= 2.000, -6.418, -3.716, -2.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000

    max_number_of_points = 21

    static_pitch= 0.000
    static_cg_height= 3.375
    gear_system_type=1 //Electric

    [gear_warning_system]
    gear_warning_available = 1 //Normal
    pct_throttle_limit = 0.1 //Percent throttle that activates warning
    flap_limit_idle = 0.0 //Flap angle that activates warning at idle
    flap_limit_power = 16.0 //Flap angle that activates warning at above idle

    [brakes]
    parking_brake = 1 //Parking brake available
    toe_brakes_scale = 1.0 //Brake scalar

    [hydraulic_system]
    normal_pressure = 3000.0 //PSI
    electric_pumps = 0 //no electric pumps
    engine_map = 1,0,0,0 //pumps on Eng1

    [Views]
    eyepoint= -3.95, -0.85, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum

    [Radios]
    // Radio Type = availiable, standby frequency, has glide slope
    Audio.1 = 1
    Com.1 = 1, 1
    Com.2 = 1, 1
    Nav.1 = 1, 1, 1
    Nav.2 = 1, 1, 0
    Adf.1 = 1
    Transponder.1 = 1
    Marker.1 = 1

    [LIGHTS]
    //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
    light.0 = 3, -4.31, -9.47, -1.07, fx_navred
    light.1 = 3, -4.31, 9.48, -1.07, fx_navgre
    light.2 = 2, -9.55, -3.40, 0.91, fx_strobe
    light.3 = 2, -9.55, 3.40, 0.91, fx_strobe
    light.4 = 1, 0.00, 0.00, -1.55, fx_beacon
    light.5 = 4, 0.00, 0.00, -1.55, fx_vclight

    [keyboard_response]
    //Breakpoint speeds (knots) on the keyboard increments of control surfaces.
    //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
    elevator = 100, 180
    aileron = 200, 1000
    rudder = 200, 1000

    [direction_indicators]
    //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
    //2 Indicator number of slaving indicator if Type = 4
    turn_indicator.0=1,1 //Turn AND Bank
    direction_indicator.0=1,0

    [attitude_indicators]
    //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
    attitude_indicator.0 = 1

    [turn_indicators]
    //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
    turn_indicator.0=1,0

    [EFFECTS]
    wake=fx_wake
    water=fx_spray
    dirt=fx_tchdrt
    concrete=fx_sparks
    touchdown=fx_tchdwn_s, 1

    [fuel]
    LeftMain = -3.689, -2.767, -1.240, 5.000, 0.000
    RightMain = -3.689, 2.767, -1.240, 5.000, 0.000
    fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
    number_of_tank_selectors = 1
    electric_pump=1
    Center1= -1.020, 0.000, 0.699, 10.000, 0.000

    [airplane_geometry]
    wing_area = 123.000
    wing_span = 19.000
    wing_root_chord = 10.070
    wing_dihedral = 1.700
    wing_incidence = 0.000
    wing_twist = -3.000
    oswald_efficiency_factor= 0.680
    wing_winglets_flag = 0
    wing_sweep = 38.400
    wing_pos_apex_lon = 0.560
    wing_pos_apex_vert = -0.839
    htail_area = 13.690
    htail_span = 6.550
    htail_pos_lon = 7.451
    htail_pos_vert = 0.399
    htail_incidence = 0.000
    htail_sweep = 0.000
    vtail_area = 18.377
    vtail_span = 4.458
    vtail_sweep = 57.000
    vtail_pos_lon = -7.336
    vtail_pos_vert = 0.000
    elevator_area = 2.550
    aileron_area = 5.012
    rudder_area = 7.668
    elevator_up_limit = 27.000
    elevator_down_limit = 29.000
    aileron_up_limit = 20.000
    aileron_down_limit = 15.000
    rudder_limit = 20.000
    elevator_trim_limit = 10.000
    spoiler_limit = 0.000
    spoilerons_available = 0
    aileron_to_spoileron_gain = 0.000
    min_ailerons_for_spoilerons = 0.000
    min_flaps_for_spoilerons = 0.000




    [Reference Speeds]
    flaps_up_stall_speed = 48.000
    full_flaps_stall_speed = 43.200
    cruise_speed = 129.000
    max_indicated_speed= 163.000

    [autopilot]
    autopilot_available= 1
    flight_director_available= 0
    default_vertical_speed= 700.0
    autothrottle_available= 0
    max_pitch=10.0
    max_pitch_acceleration=1.0
    max_pitch_velocity_lo_alt=2.0
    max_pitch_velocity_hi_alt=1.5
    max_pitch_velocity_lo_alt_breakpoint=20000.0
    max_pitch_velocity_hi_alt_breakpoint=28000.0
    max_bank=25.0
    max_bank_acceleration=1.8
    max_bank_velocity=3.00
    max_throttle_rate=0.10
    nav_proportional_control=9.00
    nav_integrator_control=0.25
    nav_derivative_control=0.00
    nav_integrator_boundary=2.50
    nav_derivative_boundary=0.00
    gs_proportional_control=9.52
    gs_integrator_control=0.26
    gs_derivative_control=0.00
    gs_integrator_boundary=0.70
    gs_derivative_boundary=0.00
    yaw_damper_gain = 1.0
    pitch_takeoff_ga= 8.000

    [forcefeedback]
    gear_bump_nose_magnitude=6000 ; 0 - 10000
    gear_bump_nose_direction=18000 ; 0 - 35999 degrees
    gear_bump_nose_duration=250000 ; in microseconds
    gear_bump_left_magnitude=6000 ; 0 - 10000
    gear_bump_left_direction=35500 ; 0 - 35999 degrees
    gear_bump_left_duration=250000 ; in microseconds
    gear_bump_right_magnitude=6000 ; 0 - 10000
    gear_bump_right_direction=00500 ; 0 - 35999 degrees
    gear_bump_right_duration=250000 ; in microseconds
    ground_bumps_magnitude1=3250 ; 0 - 10000
    ground_bumps_angle1=8900 ; 0 - 35999 degrees
    ground_bumps_intercept1=5.0
    ground_bumps_slope1=0.48
    ground_bumps_magnitude2=750 ; 0 - 10000
    ground_bumps_angle2=9100 ; 0 - 35999 degrees
    ground_bumps_intercept2=0.075
    ground_bumps_slope2=1.0
    crash_magnitude1=10000 ; 0 - 10000
    crash_direction1=01000 ; 0 - 35999 degrees
    crash_magnitude2=10000 ; 0 - 10000
    crash_direction2=9000 ; 0 - 35999 degrees
    crash_period2=75000 ; in microseconds
    crash_duration2=2500000 ; in microseconds

    [stall_warning]
    type=1

    [Flaps.0]
    type= 0
    span-outboard= 0.500
    extending-time= 7.000
    system_type= 0
    damaging-speed= 120.000
    blowout-speed= 150.000
    lift_scalar= 1.000
    drag_scalar= 1.000
    pitch_scalar= 1.000
    flaps-position.0= 0.000, 0.000
    flaps-position.1= 12.700, 0.000
    flaps-position.2= 25.300, 0.000
    flaps-position.3= 38.000, 0.000
    [fltsim.1]
    title=Vari Viggan 27
    sim=SingleEngineProp
    model=
    panel=Main
    panel_alias=c172\panel
    sound=
    sound_alias=c172\sound
    texture=
    kb_checklists=
    kb_reference=
    atc_id=N27VV
    ui_manufacturer=Rutan Aircraft Factory
    ui_type=SingleEngineProp
    ui_variation=Main Panel
    description=Average panel set-up for the Vari-Viggan Model 27
    atc_heavy=0
    atc_airline=
    atc_flight_number=
    [fltsim.2]
    title=VV 27 Typ
    sim=SingleEngineProp
    model=
    panel=VV27
    panel_alias=c172\panel
    sound=
    sound_alias=c172\sound
    texture=
    kb_checklists=
    kb_reference=
    atc_id=N27VV
    ui_manufacturer=Rutan Aircraft Factory
    ui_type=SingleEngineProp
    ui_variation=VV27 Typical
    description=To Follow
    atc_heavy=0
    atc_airline=
    atc_flight_number=
    [fltsim.3]
    title=VV27
    sim=SingleEngineProp
    model=
    panel=VV27 Main
    panel_alias=c172\panel
    sound=
    sound_alias=c172\sound
    texture=
    kb_checklists=
    kb_reference=
    atc_id=N27VV
    ui_manufacturer=Rutan Aircraft Factory
    ui_type=SingleEngineProp
    ui_variation=Typival VV27 Panel
    description=coming
    atc_heavy=0
    atc_airline=
    atc_flight_number=

  8. Default

    I'm sorry for the delay in my reply...I missed the fact that you had posted your .cfg!
    I note that your datum position is the same as your cg position. That's okay as long as your cg is correct. Any chance you could grab a screen out of Gmax that shows the plane with the "home grid" active?

  9. #9

    Default

    Sorry for [I]my[I] delay. Here's the shot.
    Click image for larger version. 

Name:	VV27.jpg 
Views:	14 
Size:	174.3 KB 
ID:	128033
    Hope this helps.
    By the way, CG was determined from the 18% scale RC plans.
    Last edited by jwgk1; 06-07-2012 at 06:12 PM.

  10. #10

    Default

    N2056: Are you out there?

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