Mikoyan-Gurevich MiG-15

施加於模型產出的一切、在裝置上限之前的最終整體輸出縮放。

設定理由: Scales overall profile strength while preserving effect balance, subject to device and output limits.

把搖桿拉回中央的基礎回中力。其他所有力都疊加在它之上。太低,正常飛行中搖桿會發軟;太高,它會與你的手較勁,並掩蓋疊加其上的細微提示。

設定理由: This profile uses reversible-control loading for Mikoyan-Gurevich MiG-15. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 65 KIAS.

中央附近彈簧保持安靜的小中立區,讓靜止時的微小移動不會咔嗒作響。更寬更安穩但更松,更窄更精確但可能在中央附近抖動。

設定理由: Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.

作用於兩條持續軸載荷的主縮放,在它們各自的獨立平衡之前施加。設定檔通常不動它,而是調校兩條軸載荷。

設定理由: The aerodynamic-load gain is 0.8 with an indicated-speed reference of 230 KIAS. This supplies speed-dependent loading alongside the spring.

啟用低速彈簧介入視窗(上面的起始/全強度節數)。關閉時彈簧在所有速度下恆定。

設定理由: Allows baseline spring strength to rise with indicated airspeed where the control law permits it.

在靜止、空速尚未產生氣動力之前,彈簧還剩多少。下限高,停機時搖桿結實;下限低,則是停放輕型飛機那種鋼索鬆弛的感覺。

設定理由: Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.

彈簧從低速下限開始向全強度攀升的空速:起飛滑跑中操縱面"甦醒"的那一刻。

設定理由: Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.

彈簧達到全強度的空速。從起點到這裡,隨著氣流在操縱面上增強,回中逐漸變硬。

設定理由: Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.

氣動載荷達到設計滿值的指示空速。它把整條載荷曲線錨定在飛機真實的速度範圍:172在110節就載滿,噴氣機要晚得多。

設定理由: Sets the IAS reference for aerodynamic loading. It is an estimate, not published cruise TAS or a flight limit.

在偏轉載荷之外,回中本身隨速度變硬的程度。零則中央手感恆定;越大,巡航時回中越硬,起落航線上越松。

設定理由: The high-speed spring-stiffening gain is 0.15. It strengthens the permitted spring response above 65 KIAS, with the squared-speed ratio capped at 5.

速度驅動的中央變硬上限,防止高速飛行把彈簧無限上緊。

設定理由: Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.

由副翼偏轉和空速產生的持續橫滾載荷,獨立於俯仰調校。與升降舵載荷一起,決定評測中常說的操縱協調比。

設定理由: Roll and pitch aerodynamic scales are 0.72 and 1, respectively. They set the aerodynamic axis balance. No custom spring-travel curve is enabled.

由升降舵偏轉和空速產生的持續俯仰載荷,獨立於橫滾調校。這是決定機型俯仰重量的主槓桿。它不影響副翼、彈簧、配平或抖振力。

設定理由: Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.

每個穩態俯仰或橫滾力到達裝置前的上限,防止猛烈機動中砸擊或飽和硬體。

設定理由: Caps directed-force output. Native spring effects and device limits remain separate.

升降舵配平緩解持續俯仰力、移動桿的安定位置的強度。在100 %時,配平得當的飛機不需要保持壓力——正是真實飛行中"用配平消掉載荷"的流程。

設定理由: The profile uses the trim behaviour configured below. Pitch relief is off, with stored authority 0; roll authority is 0.

橫滾配平的同類緩解。多數通航機型沒有真正的副翼配平,所以保持為零;有橫滾配平的機型獲得相應的值。

設定理由: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.

由輪速和地面型別(鋪裝、草地、礫石)產生的滾動振動。

設定理由: Sets rolling texture strength, modified by speed, surface and undercarriage configuration.

來自伸縮縫、車轍和粗糙地面的短促離散顛簸,為持續隆隆聲打上標點。

設定理由: Sets gear-bump texture during ground motion, separate from touchdown impact.

接近失速及失速警告響起時的機體抖動:這副機翼宣告不滿的音量。斷失乾脆的機型抖振收斂,讓喇叭承擔警告。

設定理由: Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.

接近馬赫極限的跨音速抖振。對接近MMO的噴氣機有意義,對到不了那裡的活塞機和渦槳機為零。

設定理由: Sets high-Mach buffet strength; onset and full-strength thresholds are separate.

襟翼伸入氣流後機體的低頻振動,發生在它們真正做功的速度視窗內。

設定理由: Sets flap buffet at the configured position and speed gates. Flap movement texture is separate.

可收放起落架懸在氣流中引起的機體鼓振。固定起落架機型為零,它們的機體外形從不改變。

設定理由: Sets gear aerodynamic buffet; movement and ground-contact cues are separate.

由飛機自身失速警告系統觸發的專用抖桿器振動。只有真有抖桿器的機型才有值;其餘全靠氣動抖振和喇叭。

設定理由: Sets triggered shaker strength; inactive while the shaker feature is disabled.

機輪觸及跑道那一下的單次衝擊,按下沉率縮放:輕柔著陸是耳語,結實到達是一記悶響。

設定理由: Sets landing-impact strength; landing telemetry and response shape determine the pulse.

反推或槳葉beta區工作時的滑跑振動。無反推機型為零。

設定理由: Sets reverse-thrust vibration with valid reverser and engine conditions. Zero removes the cue.

從慢車到全功率跟隨轉速的持續動力裝置振動——前方有東西在燒油的永恆提醒。

設定理由: Sets estimated engine vibration using configured telemetry and response, not measured cockpit vibration.

僅在模擬器報告襟翼舵面確實移動時的持續振動。它跟隨真實作動器的運動和故障,而非估算的計時器。

設定理由: Sets texture from observed flap movement; a command without movement does not establish the cue.

自動駕駛指令可以讓桿實際移動多遠。在MSFS中保持極小,因為移動的軸可能被讀回為飛行員輸入;零則完全停用跟隨。

設定理由: Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.

Whether this feature is active in this profile.

設定理由: Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.

Whether this feature is active in this profile.

設定理由: Allows trim relief with supported control law and valid telemetry. Axis authorities set its amount.

Whether this feature is active in this profile.

設定理由: Enables local force trim, separate from aircraft-owned trim and add-on integration qualification.

Whether this feature is active in this profile.

設定理由: Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.

Whether this feature is active in this profile.

設定理由: Enables rate damping with the configured coefficients and control law.

Whether this feature is active in this profile.

設定理由: Autopilot following is off; the configured spring and load retain the hardware feel.

Whether this feature is active in this profile.

設定理由: Permits centering hold during a supported AP state, separate from following a moving target.

設定理由: Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.

Whether this feature is active in this profile.

設定理由: Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.

Where this effect reaches full strength (or has fully faded, for washouts).

設定理由: Sets the final flap index for detent normalization. UP plus three detents uses maximum index3.

Where this effect begins fading in.

設定理由: Sets the first flap detent that admits buffet; this is a handle index, not degrees.

Whether this feature is active in this profile.

設定理由: Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.

Whether this feature is active in this profile.

設定理由: Enables ground effects; each still needs its own strength and contact or motion telemetry.

Whether this feature is active in this profile.

設定理由: Enables engine cues with nonzero settings and valid running-engine telemetry.

Whether this feature is active in this profile.

設定理由: Enables accessory cues with configured strengths and observed accessory movement.

The strength of this effect.

設定理由: Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.