> > When the wings are level and the actuator (roll trim) stays out of > saturation, this PI controller works great. It does not grow > a bias as > long as the actuator is able to do it's job, it only grows a > bias when the > actuator does not have enough power (deflection angle) to do it's job. > > The solution to this is to stop the intergation when the > actuator goes > into saturation. > > Knowing nothing about the jsbsim structure, and only a little about PID control, could you arrange the control loop so that the Integral term is only updated when the output is between 2% and 98%?
Richard _______________________________________________ Flightgear-devel mailing list [EMAIL PROTECTED] http://mail.flightgear.org/mailman/listinfo/flightgear-devel
