Eurocopter EC135
Eurocopter EC135: The cyclic response works around an aircraft-owned neutral where the integration provides it.
Aircraft and simulator scope
- Eurocopter EC135 · MSFS 2024 · family starting point
- Eurocopter EC135 · MSFS 2020 · family starting point
Eurocopter EC135 · HPG's version 1.4 update concerns its H135 simulator, with distinct Advanced and Basic flight modes.
The simulator model and controls
The EC135, later renamed H135, developed from the MBB Bo 108 programme. Its enclosed tail rotor, twin turbines and practical cabin made it a useful platform for emergency services and other operators. The type first flew in 1994 and entered service in 1996.
This starting point selects Eurocopter EC135. Its aircraft-level settings do not select a particular developer’s custom systems.
How this profile feels
The cyclic response works around an aircraft-owned neutral where the integration provides it. Spring resistance builds with the selected airspeed response. A separate aerodynamic term adds speed-dependent control load. Cyclic damping adds resistance to hardware motion.
Plugin-written trim describes the control neutral, separately from AP engagement. Local force trim is off. Autopilot following is off.
Controls and trim
The EC135 implementation owns its trim/AFCS neutral and separately treats centered controls and FFB hardware. Its published FFB mode uses plugin-written trim references independently of autopilot servo state. Versioned AFCS and trim-release changes belong to the exact add-on generation.
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.
What the documentation establishes
HPG's version 1.4 update concerns its H135 simulator, with distinct Advanced and Basic flight modes.
The update documents simulated rotor bending, rotor blur and autorotation behavior; it does not specify the exact engine or rotor-frequency mapping.
Retreating-blade stall is specifically enabled in Advanced mode. This supports a qualitative mode-dependent effect, without a measured vibration amplitude.
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
ReviewedThis starting point selects Eurocopter EC135. Its aircraft-level settings do not select a particular developer’s custom systems.
Flight controls
Not yet reviewedThe EC135 implementation owns its trim/AFCS neutral and separately treats centered controls and FFB hardware. Its published FFB mode uses plugin-written trim references independently of autopilot servo state. Versioned AFCS and trim-release changes belong to the exact add-on generation.
Trim
Not yet reviewedPlugin-written trim describes the control neutral, separately from AP engagement. Local force trim is off. Autopilot following is off.
Autopilot and stability
Not yet reviewedAutopilot following is off; the configured spring and load retain the hardware feel.
Equipment
ReviewedGear, flap and ground cues follow the selected settings and available simulator-reported states.
Speeds and limits
Not yet reviewedThe indicated-speed references set the profile response scale; they are separate from aircraft operating limits.
Simulator integration
Not yet reviewedThe profile targets msfs2024, msfs2020. Add-on-specific controls use only the supported references configured by this profile.
Force-feedback settings
ReviewedThe 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 | What it controls and whyThe cyclic response works around an aircraft-owned neutral where the integration provides it. The baseline spring is 0. Its low-speed blend reaches baseline strength at 60 KIAS. georgl.info ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ developer.x-plane.com ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ www.hypeperformancegroup.com ↗ www.hypeperformancegroup.com ↗ |
| 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 value0.35 | What it controls and whyThe aerodynamic-load gain is 0.35 with an indicated-speed reference of 120 KIAS. This supplies speed-dependent loading alongside the spring. |
| Force tuning speed/reference | Starting value120.0 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 value60.0 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 value1 | What it controls and whyRoll and pitch aerodynamic scales are 1 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 valueDisabled | What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| Trim relief | Starting valueDisabled | 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 | What it controls and whyThe cyclic response works around an aircraft-owned neutral where the integration provides it. The baseline spring is 0. Its low-speed blend reaches baseline strength at 60 KIAS. georgl.info ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ developer.x-plane.com ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ www.hypeperformancegroup.com ↗ www.hypeperformancegroup.com ↗ |
| Spring deadband | Starting value0.02 | What it controls and whySets travel around the centre before the baseline spring resists. Smaller values engage it sooner. |
| Profile force gain | Starting value0.35 | What it controls and whyThe aerodynamic-load gain is 0.35 with an indicated-speed reference of 120 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 value1 | 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 value16.8 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 value60.0 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 value120.0 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 | What it controls and whyAdds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase. |
| 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 value1 | What it controls and whyRoll and pitch aerodynamic scales are 1 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 valueDisabled | What it controls and whyRetained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement. |
| Trim relief | Starting valueDisabled | What it controls and whyAllows trim relief with supported control law and valid telemetry. Axis authorities set its amount. |
| Elevator Authority | Starting value0.3 | What it controls and whyScales supported pitch-trim relief and permitted centre movement. Zero removes pitch response. |
| Aileron Authority | Starting value0.3 | 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 whyPlugin-written trim describes the control neutral, separately from AP engagement. Local force trim is off. The stored latch parameters are inactive; the profile does not supply a local hold-where-left neutral. georgl.info ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ www.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ developer.x-plane.com ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ skcrftrepo.rotorsim.de ↗ www.hypeperformancegroup.com ↗ www.hypeperformancegroup.com ↗ |
| GLoad Enabled | Starting valueDisabled | 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 value0.05 | 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 | 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 value1 | What it controls and whySets the final flap index for detent normalization. UP plus three detents uses maximum index3. |
| Minimum flap index | Starting value1 | What it controls and whySets the first flap detent that admits buffet; this is a handle index, not degrees. |
| Gain | Starting value0 | 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 | What it controls and whySets rolling texture strength, modified by speed, surface and undercarriage configuration. |
| Gain | Starting value0 | What it controls and whySets gear-bump texture during ground motion, separate from touchdown impact. |
| Gain | Starting value0.5 | What it controls and whySets landing-impact strength; landing telemetry and response shape determine the pulse. |
| Gain | Starting value0 | 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 value0.06 | 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 | What it controls and whySets texture from observed flap movement; a command without movement does not establish the cue. |
| Gain | Starting value0 | What it controls and whySets texture from observed gear movement, separate from aerodynamic and touchdown effects. |
Limits and open questions
- Changes to pedal authority describe simulator handling, without establishing real cyclic servo loading or linkage.
- The update mentions visual trim tabs, without identifying a pilot trim or force-neutral mechanism.
- No applicable automatic-flight description appears in the retained update or tag archive.
- Low-speed yaw improvements supply no airspeed schedule or indicated-air-speed loading reference.
- No cyclic, trim or autopilot telemetry contract is published in these update pages.
- Eurocopter EC135 documentary evidence does not establish force-feedback hardware acceptance.
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.