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The electrical power logic appears to having some strange behaviour.
The bus init state do not match between 2020 and 2024. In 2024, all the busses in the infinitbat are connected by default.
Init State of 2020
Init state of 2024
Odd logic of the ESS BAT switch
When using the ESS BAT switch, the state of the DC_ESS_BUS and AC_ESS_BUS is only toggled when the ESS BAT switch is in the ON position. This is instead of following the ON-OFF state of the ESS BAT switch. Thus two clicks (OFF->ON) are required to toggle the state of the ESS BAT. Therefore, it is possible to create a situation where the
After applying EXT PWR, it appears the AC and DC ESS BUS can't both be powered at the same time. They get stuck in an alternate state based on the true state of the ESS BAT from the previous step.
Expected behavior
Electrical busses should be powered correctly based on the electrical bus logic. Aircraft should init with the electrical busses powered off when all ext power and battery are disconnected.
Steps to reproduce
Load aircraft in 2024. Open the behaviour panel and inspect the electrical debug.
Observe the initial electrical state and observe how the state changes while connecting batteries and external power.
References (optional)
No response
Additional info (optional)
No response
Discord Username (optional)
Heclak
The text was updated successfully, but these errors were encountered:
Aircraft Version
Development
Build info
Describe the bug
This bug is isolated to MSFS2024
The electrical power logic appears to having some strange behaviour.
Init State of 2020
Init state of 2024
Odd logic of the ESS BAT switch
When using the ESS BAT switch, the state of the DC_ESS_BUS and AC_ESS_BUS is only toggled when the ESS BAT switch is in the ON position. This is instead of following the ON-OFF state of the ESS BAT switch. Thus two clicks (OFF->ON) are required to toggle the state of the ESS BAT. Therefore, it is possible to create a situation where the
After applying EXT PWR, it appears the AC and DC ESS BUS can't both be powered at the same time. They get stuck in an alternate state based on the true state of the ESS BAT from the previous step.
Expected behavior
Electrical busses should be powered correctly based on the electrical bus logic. Aircraft should init with the electrical busses powered off when all ext power and battery are disconnected.
Steps to reproduce
References (optional)
No response
Additional info (optional)
No response
Discord Username (optional)
Heclak
The text was updated successfully, but these errors were encountered: