TOGA MU-2 Marquise 4-blade OEM
TOGA MU-2 Marquise 4-blade OEM: The spoiler-based lateral system motivates its own axis balance.
Aircraft and simulator scope
- TOGA MU-2 Marquise 4-blade OEM · TOGA Simulations · X-Plane 12 · Add-on starting point
The simulator model and controls
The MU-2 first flew in 1963 and became a major postwar Japanese civil-aircraft programme. Two turboprops power its compact high-wing airframe, built in short- and long-fuselage versions.
This profile selects TOGA MU-2 Marquise 4-blade OEM for X-Plane 12.
How this profile feels
The spoiler-based lateral system motivates its own axis balance. Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load.
Electric trim ailerons and mechanical elevator trim are separate from AP pitch attitude. Valid trim provides the configured pressure relief. Autopilot following is off.
Controls and trim
The MU-2 uses mechanically commanded roll spoilers and separate electrically trimmed ailerons. Elevator trim is mechanical. The autopilot’s TCS releases servos and its pitch wheel commands attitude, distinct from the elevator trim control.
The selected implementation
TOGA separates four/five-blade propellers and OEM/GNS/G600 panels; G600 requires its own display package and retains the SPZ500.
About the values
The gains are normalized profile settings. They describe the chosen effect balance; hand force depends on the device and its output limits. IAS references are tuning values rather than operating limits. Physical acceptance of this revision remains pending.
Documentary review and sources
These decisions describe the documentary basis and remaining gaps for this revision. Aircraft documentation and a starting setting describe different kinds of evidence.
Aircraft and variant
InheritedThis profile selects TOGA MU-2 Marquise 4-blade OEM for X-Plane 12.
Flight controls
InheritedThe MU-2 uses mechanically commanded roll spoilers and separate electrically trimmed ailerons. Elevator trim is mechanical. The autopilot’s TCS releases servos and its pitch wheel commands attitude, distinct from the elevator trim control.
Trim
InheritedElectric trim ailerons and mechanical elevator trim are separate from AP pitch attitude. Pitch authority 0.25 provides load relief and permitted centre movement; roll authority is 0.1.
Autopilot and stability
InheritedAutopilot following is off; the configured spring and load retain the hardware feel.
Equipment
InheritedTOGA separates four/five-blade propellers and OEM/GNS/G600 panels; G600 requires its own display package and retains the SPZ500.
Speeds and limits
InheritedThe indicated-speed references set the profile response scale; they are separate from aircraft operating limits.
Simulator integration
InheritedThe profile targets xplane12. Add-on-specific controls use only the supported references configured by this profile.
Force-feedback settings
InheritedThe settings define the profile’s effect balance. Device output limits affect physical hand force.
Starting settings and their rationale
These configured values are starting estimates. The explanations describe what each setting controls; physical validation appears separately below.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Spring strength | Starting value0.72 | What it controls and whyThe spoiler-based lateral system motivates its own axis balance. The baseline spring is 0.72. Its low-speed blend reaches baseline strength at 100 KIAS. |
| Master force gain | Starting value0.85 | What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits. |
| Profile force gain | Starting value0.64 | What it controls and whyThe aerodynamic-load gain is 0.64 with an indicated-speed reference of 220 KIAS. This supplies speed-dependent loading alongside the spring. |
| Force tuning speed/reference | Starting value220 kt | What it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| Spring response reference speed | Starting value100 kt | What it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Aileron force scale | Starting value0.85 | What it controls and whyRoll and pitch aerodynamic scales are 0.85 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Elevator force scale | Starting value1 | What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Trim feel | Starting valueEnabled | What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| Trim relief | Starting valueEnabled | What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| Autopilot follow | Starting valueDisabled | What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel. |
| Autopilot neutral hold | Starting valueDisabled | What it controls and whyPermits centering hold during a supported AP state, separate from following a moving target. |
| Output force limit | Starting value0.55 | What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate. |
All 44 starting settings and their rationale
The settings define the profile’s effect balance. Device output limits affect physical hand force.
| Setting | Starting value | What it controls and why |
|---|---|---|
| Spring strength | Starting value0.72 | What it controls and whyThe spoiler-based lateral system motivates its own axis balance. The baseline spring is 0.72. Its low-speed blend reaches baseline strength at 100 KIAS. |
| Spring deadband | Starting value0.05 | What it controls and whySets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Profile force gain | Starting value0.64 | What it controls and whyThe aerodynamic-load gain is 0.64 with an indicated-speed reference of 220 KIAS. This supplies speed-dependent loading alongside the spring. |
| Master force gain | Starting value0.85 | What it controls and whyScales overall profile strength while preserving effect balance, subject to device and output limits. |
| QBlend Enabled | Starting valueEnabled | What it controls and whyAllows baseline spring strength to rise with indicated airspeed where the control law permits it. |
| QSpring Minimum Factor | Starting value0.55 | What it controls and whySets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
| QSpring Start Knots | Starting value25 kt | What it controls and whySets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit. |
| Spring response reference speed | Starting value100 kt | What it controls and whySets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
| Force tuning speed/reference | Starting value220 kt | What it controls and whySets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit. |
| Airspeed spring stiffening gain | Starting value0.1 | What it controls and whyThe high-speed spring-stiffening gain is 0.1. It strengthens the permitted spring response above 100 KIAS, with the squared-speed ratio capped at 5. |
| Airspeed spring stiffening limit | Starting value5 | What it controls and whyLimits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
| Aileron force scale | Starting value0.85 | What it controls and whyRoll and pitch aerodynamic scales are 0.85 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled. |
| Elevator force scale | Starting value1 | What it controls and whyScales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
| Output force limit | Starting value0.55 | What it controls and whyCaps directed-force output. Native spring effects and device limits remain separate. |
| Trim feel | Starting valueEnabled | What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| Trim relief | Starting valueEnabled | What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| Elevator Authority | Starting value0.25 | What it controls and whyElectric trim ailerons and mechanical elevator trim are separate from AP pitch attitude. Pitch authority 0.25 provides load relief and permitted centre movement; roll authority is 0.1. |
| Aileron Authority | Starting value0.1 | What it controls and whyScales supported roll-trim relief and permitted centre movement. Zero removes roll response. |
| Force Trim Enabled | Starting valueDisabled | What it controls and whyEnables local force trim, separate from aircraft-owned trim and add-on integration qualification. |
| GLoad Enabled | Starting valueEnabled | What it controls and whyAllows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it. |
| Rate Damping Enabled | Starting valueEnabled | What it controls and whyEnables rate damping with the configured coefficients and control law. |
| Autopilot follow | Starting valueDisabled | What it controls and whyAutopilot following is off; the configured spring and load retain the hardware feel. |
| Autopilot follow authority | Starting value0.1 | What it controls and whySets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply. |
| Autopilot neutral hold | Starting valueDisabled | What it controls and whyPermits centering hold during a supported AP state, separate from following a moving target. |
| Autopilot neutral hold strength | Starting value0.6 | What it controls and whySets admitted AP neutral-hold strength; inactive while neutral hold is disabled. |
| Enabled | Starting valueEnabled | What it controls and whyEnables aerodynamic cues; each still needs nonzero strength and its simulator conditions. |
| Gain | Starting value0.25 | What it controls and whySets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
| Gain | Starting value0 | What it controls and whySets high-Mach buffet strength; onset and full-strength thresholds are separate. |
| Gain | Starting value0 | What it controls and whySets flap buffet at the configured position and speed gates. Flap movement texture is separate. |
| Maximum flap index | Starting value3 | What it controls and whySets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
| Minimum flap index | Starting value2 | What it controls and whySets the first flap detent that admits buffet; this is a handle index, not degrees. |
| Gain | Starting value0.055 | What it controls and whySets gear aerodynamic buffet; movement and ground-contact cues are separate. |
| Shaker Enabled | Starting valueDisabled | What it controls and whyPermits shaker at supported warning conditions; the switch does not establish aircraft equipment. |
| Stick shaker amplitude | Starting value0.5 | What it controls and whySets triggered shaker strength; inactive while the shaker feature is disabled. |
| Enabled | Starting valueEnabled | What it controls and whyEnables ground effects; each still needs its own strength and contact or motion telemetry. |
| Gain | Starting value0.24 | What it controls and whySets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Gain | Starting value0.18 | What it controls and whySets gear-bump texture during ground motion, separate from touchdown impact. |
| Gain | Starting value0.4 | What it controls and whySets landing-impact strength; landing telemetry and response shape determine the pulse. |
| Gain | Starting value0.14 | What it controls and whySets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue. |
| Enabled | Starting valueEnabled | What it controls and whyEnables engine cues with nonzero settings and valid running-engine telemetry. |
| Gain | Starting value0.07 | What it controls and whySets estimated engine vibration using configured telemetry and response, not measured cockpit vibration. |
| Enabled | Starting valueEnabled | What it controls and whyEnables accessory cues with configured strengths and observed accessory movement. |
| Gain | Starting value0.055 | What it controls and whySets texture from observed flap movement; a command without movement does not establish the cue. |
| Gain | Starting value0.06 | What it controls and whySets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
Limits and open questions
- Force amplitudes, damping and response curves are editable estimates, not measured hand forces. Installed and physical checks remain deferred.
- No custom servo target, failure, control-lock or maintenance-state interface is inferred. AP follow and neutral hold are off; the simulator retains aircraft control authority.
- Original radio-navigation stack with SPZ500; no GPSS converter assumed.
- Roll-spoiler hinge forces and independent left/right trim-aileron failures are not separately modelled; ordinary aileron-surface follow and generic speedbrake effects are disabled.
- Pulsed/delayed flaps use actual motion only. Sustained actual-only flap cues require a separately versioned policy; missing surface telemetry cannot be replaced with a claimed actuator state.
- Old overview prose discusses a future XP12 port, but current publisher and version2.1 notes confirm XP12 release. Linked2.2 notes return404; no2.2 release inferred.
- Overview table repeats MU2B60_4B_GNS.acf for the 5-blade GNS row; the described 5B naming convention is used provisionally. Matching needs explicit developer and variant or a saved aircraft-default binding.
Physical validation
No physical force validation is recorded in this public catalogue for this revision. Documentary review and software checks do not establish how a particular device feels.