| Spring strength | 0.55 | The inherited 0.55 spring supplies a fixed centre. Low-speed airspeed blending and high-speed stiffening are disabled. |
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| Spring deadband | 0.04 | Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
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| Force gain | 0.04 | The 0.04 gain adds a small aerodynamic-load term alongside the fixed-centre spring. It does not reproduce the guide’s commanded-G law. |
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| Master gain | 0.85 | Scales overall profile strength while preserving effect balance, subject to device and output limits. |
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| Dynamic-pressure blend | False | Allows baseline spring strength to rise with indicated airspeed where the control law permits it. |
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| Minimum spring factor | 0.5 | Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength. |
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| Spring wake-up speed | 20 kt | Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit. |
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| Spring full-strength speed | 90 kt | Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it. |
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| Velocidad de ajuste de fuerza | 300.0 kt | The retained 300-KIAS reference is the profile’s aerodynamic load scale; it is not a published F-117 cruise speed or limit. |
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| Airspeed spring stiffening | 0 | Adds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase. |
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| Airspeed stiffening cap | 5 | Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap. |
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| Aileron force scale | 1 | Scales roll aerodynamic loading. The separate roll spring curve also affects total axis balance. |
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| Elevator force scale | 1 | Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings. |
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| Maximum output force | 0.55 | Caps directed-force output. Native spring effects and device limits remain separate. |
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| StickFeel · Trim feel enabled | False | Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
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| StickFeel · Trim relief enabled | False | Trim relief is disabled. The guide’s simulator trim adjustment does not establish a physical neutral-to-trim relationship. |
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| StickFeel · Elevator authority | 0.3 | The stored pitch authority is inactive because trim relief is disabled; simulator trim does not move the hardware neutral through this effect. |
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| StickFeel · Aileron authority | 0.3 | Scales supported roll-trim relief and permitted centre movement. Zero removes roll response. |
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| StickFeel · Force trim enabled | False | Enables local force trim, separate from aircraft-owned trim and add-on integration qualification. |
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| StickFeel · G load enabled | False | Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it. |
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| StickFeel · Rate damping enabled | True | Enables rate damping with the configured coefficients and control law. |
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| Autopilot · Follow enabled | False | The guide’s autopilot has altitude, pitch-based Mach, heading and destination/navigation modes. Mach hold changes pitch rather than throttle. The guide does not publish calibrated servo targets, so physical autopilot following and neutral hold stay off. |
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| Autopilot · Follow authority | 0.05 | Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply. |
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| Autopilot · Neutral hold enabled | False | Permits centering hold during a supported AP state, separate from following a moving target. |
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| Autopilot · Neutral hold strength | 0.6 | Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled. |
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| Aero · Enabled | True | Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions. |
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| Aero · Gain | 0.15 | Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings. |
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| Aero · Gain | 0 | Sets high-Mach buffet strength; onset and full-strength thresholds are separate. |
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| Aero · Gain | 0 | Flap buffet is disabled; conventional flap behavior is not inferred from the shared force parent. |
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| Aero · Max flap index | 2 | Sets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
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| Aero · Min flap index | 2 | Sets the first flap detent that admits buffet; this is a handle index, not degrees. |
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| Aero · Gain | 0.1 | Sets gear aerodynamic buffet; movement and ground-contact cues are separate. |
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| Aero · Shaker enabled | False | Permits shaker at supported warning conditions; the switch does not establish aircraft equipment. |
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| Aero · Amplitude | 0.5 | Sets triggered shaker strength; inactive while the shaker feature is disabled. |
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| Ground · Enabled | True | Enables ground effects; each still needs its own strength and contact or motion telemetry. |
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| Ground · Gain | 0.36 | Sets rolling texture strength, modified by speed, surface and undercarriage configuration. |
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| Ground · Gain | 0.3 | Sets gear-bump texture during ground motion, separate from touchdown impact. |
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| Ground · Gain | 0.88 | Sets landing-impact strength; landing telemetry and response shape determine the pulse. |
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| Ground · Gain | 0 | Reverse-thrust vibration is disabled. |
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| Engine · Enabled | False | Enables engine cues with nonzero settings and valid running-engine telemetry. |
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| Engine · Gain | 0 | Engine rumble is off, alongside simulator engine-vibration following. No measured F-117 engine or afterburner vibration is assigned. |
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| Mechanical · Enabled | True | Enables accessory cues with configured strengths and observed accessory movement. |
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| Mechanical · Gain | 0 | Flap-motion texture is disabled. |
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| Mechanical · Gain | 0.12 | Sets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
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| StickAlive · Enabled | False | This independently configured effect remains subject to valid simulator telemetry and bounded device output. |
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| StickAlive · Use sim engine vibration | False | This independently configured effect remains subject to valid simulator telemetry and bounded device output. |
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| Hydraulics · Loss load increase | 0 | Hydraulic-loss loading is zero. An aircraft-specific F-117 failure-to-inceptor response has not been established. |
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| Aero · Gain | 0 | Spoiler buffet is disabled; a spoiler cue is not inferred from the shared force parent. |
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| AeroDrag · Gain | 0 | This independently configured effect remains subject to valid simulator telemetry and bounded device output. |
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| AeroDrag · Gain | 0 | This independently configured effect remains subject to valid simulator telemetry and bounded device output. |
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| Mechanical · Gain | 0 | Discrete flap-step texture is disabled. |
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| Mechanical · Gain | 0 | Flap-arrival texture is disabled. |
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