Version: SU4 - 1.6.34.0 and SU5 Beta - 1.7.11.0
Frequency: Consistently
Severity: Low/High
Context: Custom C152 variant in all contexts, default DA62, and others.
Bug description:
Expected: When consuming more power than the alternator/generator is configured to supply, the generator supplies 100% of its ability and the battery gracefully supplies the rest, battery starts to discharge.
Current behavior: When consuming more power than the generator is configured to supply, and the generator output voltage is below the battery voltage, the generator supply starts to very rapidly flicker between high load and no load. The battery very rapidly flickers between no load/discharging. Animations and behavior like low voltage lights and low voltage pfd warnings also rapidly flicker.
Workaround: Giving the aircraft a massively overrated generator so it’s never overloaded, like some of the default aircraft. This is unfortunate.
Am I misunderstanding the expected behavior?
Secondary question: I also don’t think the throttle/RPM is affecting the alternator output?
Repro steps:
- In my privately sent package, load the C152 variant “DUCKY” in ready to take off config. This version is specifically configured with a weaker generator that will reach 100% capacity when all lights are on.
- Open electrical debug and look at both the battery details and the alternator details, and also look at the right hand side of the dashboard where you find the low voltage light and ammeter.
- Turn on all lights including taxi and landing lights.
- Observe components panicking and low voltage light flickering.
- Load the default DA62 in ready to take off config.
- In the electrical debug disconnect the RH_alternator so only the LH_alternator is powering the aircraft.
- Push and hold one of the engine starter buttons and observe that the “LOW VOLTAGE” warning on the PFD is rapidly flickering, with the electrical debug view showing the alternator and battery loads are freaking out.
- Note that this will not happen if the battery voltage is lower than the alternator output voltage at the time of the test. Increase and reduce the battery charge level to observe this.
Attachments:
Testing with privatecontent 152 variant:
Testing with default DA62:
Private attachments: Send a PM to @PrivateContent with the link to this topic and the link to download your content