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The USV was presented as a recurrent neural-network model and the simulation results show that NMPC autopilot scheme outperforms its PID alternative.
A second-order sliding structure with a second-order sliding mode (SOSM) including a high-order sliding mode (HOSM) observer for the estimation of the uncertain sliding surfaces is selected to develop an integrated guidance and autopilot scheme.
The NMPC autopilot is benchmarked against a PID autopilot scheme to guide the USV in the presence of disturbances through different line-of-sight waypoints stored in a mission planner.
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This paper describes the EFIGENIA EJ-1 Short or Vertical take-off and Landing (S/VTOL) autonomous intelligent Unmanned Aerial Vehicle (UAV) embedded multiprocessor fuzzy logic flight guidance and control system scheme autopilot system designed.
However, so is the autopilot button, and if you press it by accident, you could mess with the autopilot system.
Since different gain designs may achieve the same open-loop crossover frequency, it should be neither considered as a performance objective of the optimal autopilot design-schemes nor neglected.
The obtained results are used in the design of a control scheme for the velocity autopilot of the vehicle.
This paper concentrates on the problem of designing a three-dimensional nonlinear guidance law accounting for saturation nonlinearity and the dynamics of missile autopilot based on a command filtered backstepping (CFBS) scheme.
An adaptive backstepping control scheme is proposed to design a missile autopilot during boost-phase.
In this paper, a novel second-order sliding mode control (NSOSMC) scheme with finite time convergence is proposed for the autopilot design of skid-to-turn (STT) missiles considering coupling effects to track the desired maneuver commands.
Therefore, autopilot is not suitable in the original control system.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com