mirror of https://github.com/ArduPilot/ardupilot
585d61b960
The old code relies on the action of the integrator to raise the nose above the minimum pitch angle which depending on the model and the tuning can be too slow to correct. Biasing the pitch angle to climbout minimum will reduce the taken before an overspeed condition is corrected. |
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AP_TECS.cpp | ||
AP_TECS.h |