North American Rockwell OV-10 Bronco

施加于模型产出的一切、在设备上限之前的最终整体输出缩放。

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

把摇杆拉回中央的基础回中力。其他所有力都叠加在它之上。太低,正常飞行中摇杆会发软;太高,它会与你的手较劲,并掩盖叠加其上的细微提示。

设定理由: This profile uses reversible-control loading for North American Rockwell OV-10 Bronco. The baseline spring is 0.74. Its low-speed blend reaches baseline strength at 70 KIAS.

中央附近弹簧保持安静的小中立区,让静止时的微小移动不会咔嗒作响。更宽更安稳但更松,更窄更精确但可能在中央附近抖动。

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

作用于两条持续轴载荷的主缩放,在它们各自的独立平衡之前施加。配置文件通常不动它,而是调校两条轴载荷。

设定理由: The aerodynamic-load gain is 0.68 with an indicated-speed reference of 180 KIAS. This supplies speed-dependent loading alongside the spring.

启用低速弹簧介入窗口(上面的起始/全强度节数)。关闭时弹簧在所有速度下恒定。

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

在静止、空速尚未产生气动力之前,弹簧还剩多少。下限高,停机时摇杆结实;下限低,则是停放轻型飞机那种钢索松弛的感觉。

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

弹簧从低速下限开始向全强度攀升的空速:起飞滑跑中操纵面"苏醒"的那一刻。

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

弹簧达到全强度的空速。从起点到这里,随着气流在操纵面上增强,回中逐渐变硬。

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

气动载荷达到设计满值的指示空速。它把整条载荷曲线锚定在飞机真实的速度范围:172在110节就载满,喷气机要晚得多。

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

在偏转载荷之外,回中本身随速度变硬的程度。零则中央手感恒定;越大,巡航时回中越硬,起落航线上越松。

设定理由: The high-speed spring-stiffening gain is 0.1. It strengthens the permitted spring response above 70 KIAS, with the squared-speed ratio capped at 5.

速度驱动的中央变硬上限,防止高速飞行把弹簧无限上紧。

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

由副翼偏转和空速产生的持续横滚载荷,独立于俯仰调校。与升降舵载荷一起,决定评测中常说的操纵协调比。

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

由升降舵偏转和空速产生的持续俯仰载荷,独立于横滚调校。这是决定机型俯仰重量的主杠杆。它不影响副翼、弹簧、配平或抖振力。

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

每个稳态俯仰或横滚力到达设备前的上限,防止猛烈机动中砸击或饱和硬件。

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

升降舵配平缓解持续俯仰力、移动杆的安定位置的强度。在100 %时,配平得当的飞机不需要保持压力——正是真实飞行中"用配平消掉载荷"的流程。

设定理由: The profile uses the trim behaviour configured below. Pitch authority 0.3 provides load relief and permitted centre movement; roll authority is 0.14.

横滚配平的同类缓解。多数通航机型没有真正的副翼配平,所以保持为零;有横滚配平的机型获得相应的值。

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

由轮速和地面类型(铺装、草地、砾石)产生的滚动振动。

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

来自伸缩缝、车辙和粗糙地面的短促离散颠簸,为持续隆隆声打上标点。

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

接近失速及失速警告响起时的机体抖动:这副机翼宣告不满的音量。断失干脆的机型抖振收敛,让喇叭承担警告。

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

接近马赫极限的跨音速抖振。对接近MMO的喷气机有意义,对到不了那里的活塞机和涡桨机为零。

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

襟翼伸入气流后机体的低频振动,发生在它们真正做功的速度窗口内。

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

可收放起落架悬在气流中引起的机体鼓振。固定起落架机型为零,它们的机体外形从不改变。

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

由飞机自身失速警告系统触发的专用抖杆器振动。只有真有抖杆器的机型才有值;其余全靠气动抖振和喇叭。

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

机轮触及跑道那一下的单次冲击,按下沉率缩放:轻柔着陆是耳语,结实到达是一记闷响。

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

反推或桨叶beta区工作时的滑跑振动。无反推机型为零。

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

从慢车到全功率跟随转速的持续动力装置振动——前方有东西在烧油的永恒提醒。

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

仅在模拟器报告襟翼舵面确实移动时的持续振动。它跟随真实作动器的运动和故障,而非估算的计时器。

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

自动驾驶指令可以让杆实际移动多远。在MSFS中保持极小,因为移动的轴可能被读回为飞行员输入;零则完全禁用跟随。

设定理由: 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.

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

Whether this feature is active in this profile.

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

Whether this feature is active in this profile.

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

Whether this feature is active in this profile.

设定理由: 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.

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

Whether this feature is active in this profile.

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

Whether this feature is active in this profile.

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

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

Whether this feature is active in this profile.

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

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

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

Where this effect begins fading in.

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

Whether this feature is active in this profile.

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

Whether this feature is active in this profile.

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

Whether this feature is active in this profile.

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

Whether this feature is active in this profile.

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

The strength of this effect.

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