Abstract
In this article, equations of motion for a two-rotor airship are derived. Moreover, the problem of engine applied forces and torques is analysed, and a trajectory generator is described and implemented into a proportional–derivative control scheme. The theoretical considerations are validated by a set of simulation tests. The simulation model takes into account the structure of the drives, namely the two engines placed symmetrically on both sides of the object. The conducted simulations validate the robustness of the controller in the case of unexpected disturbance occurrence.
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