Consequently, this research addresses the general problem of designing an agent-based autonomous flight control (AFC) architecture of a UAV to facilitate autonomous routing/navigation in uncharted and unascertained environments of organized foyer surroundings. The specific problem of this research is the ...
According to Chen et al. (2009), an autonomous control architecture presents three hierarchy levels with the principle of Increasing Precision with Decreasing Intelligence (IPDI) (Saridis1989). The lowest is the execution level, with the fewest intelligence control algorithms. In the middle is the ...
The VECTOR-600 features a solid, validated architecture and is based on the accumulated experience of many thousands of flying hours on a wide variety of customer platforms. The Flight Control Computer VECTOR is suitable for: Fixed Wing UAV Platforms Rotary Wing UAV Platforms VTOL UAV Platforms. ...
Aimed at characteristics of the small unmanned aerial vehicle (UAV) with static stability, the hardware architecture and the control navigation methodology of the flight control system, which was based on ARM and FPGA were designed. The master processor ARM was used to calculate the control and na...
FIGURE I. SYSTEM ARCHITECTURE UA V is the carrier of meteorological detection systems on the basis of data link technology, under the remote control of the ground control station, it is responsible for delivery of detection system to the intended target region to detect, and the communications ...
In this architecture, formation control strategies are appropriate when a large number of unmanned aerial vehicles (UAVs) are involved. Control laws for formation control are designed based on both classical theory and inverse dynamics, and then a comparison study is performed. The effectiveness of ...
The autopilot design for the full flight envelope, starting from take-off to landing, is presented in this paper. The navigation, guidance, and flight cont
Fixed-Wing UAV Using PID Control Design. Advances in Research, 5(3), pp.1–13. Available at:http://sciencedomain.org/abstract/9899. [2]Catena, A., Melita, C.D. & Muscato, G., 2013. Automatic Tuning Architecture for the Navigation Control Loops of Unmanned Aerial Vehicles. Journal ...
Distributed architecture has been widely used in the design of reliable avionics.Distributed flight control computer designed based on Controller Area Network(CAN) is used for flight control law solution and system management of unmanned aerial vehicle(UAV).According to real-time UAV control and reliab...
A digital flight control system is developed for an Unmanned aerial vehicle. The system function and architecture are introduced in detail. To fulfill the system requirement, the control strategy is given and embedded real time flight control software is developed. The developed digital flight control...