Cruise Range Optimization of a Propeller-Driven Light Aircraft Using a Direct Transcription Method with a Regularization Term

The problem of maximizing the range of a propeller-driven aircraft in a level flight cruise is analyzed 355 maybelline fit me within the framework of optimal control.The specific fuel consumption and propeller efficiency of its propulsive system are characterized by functions of the velocity and engine power (full model), in contrast to previous wo

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