– The purpose of this article is to evaluate performance of minimum energy controllers thoroughly on a tiltrotor aircraft.
– Minimum energy controllers are designed for tiltrotor aircraft models for helicopter and airplane modes. Performance of minimum energy controllers is evaluated with respect to several criteria.
– Minimum energy controllers can be used for tiltrotor aircraft flight control system design. These controllers show satisfactory performance when noise intensities and variance bounds vary.
– Minimum energy controllers can be implemented for tiltrotor aircraft flight control system design.
– In this paper, minimum energy controllers are applied for tiltrotor aircraft flight control system design and the performance of minimum energy controllers is evaluated deeply on a complex physical system (i.e. tiltrotor aircraft).
