“…In order to obtain a range for the considered parameters, the following approaches might be adopted: - (1) obtain a nominal model of the UAV, e.g., for altitude changes only, as one of [51], include uncertainty information, see [52,53,54,55], and perform stability analysis of the uncertain system, yielding estimates of safe ranges, stabilising the closed-loop system,
- (2) for a simulation-developed model of the UAV, as used in the paper in ROS-Gazebo environment, obtained, e.g., by designing a model of the UAV in such software as Autodesk Inventor Professional 2015 (Dyson, 9.0.23.0, Autodesk, San Rafael, CA, USA), perform a series of simulations to observe the behaviour of the model in a simulation environment, as in [56],
- (3) obtain a linearized model of the UAV for the expected motion, assume possible disturbances, such as wind gusts, as bounded, an obtain stability analysis as in [57] considering ranges for controller parameters,
- (4) heuristic approach: set the ranges close to the nominal parameters of the controller, which proved to stabilise the UAV in real-world experiments.
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