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Control System for Unmanned Aerial Vehicles
"... Abstract — An open project, dealing with autopilot design for autonomous Unmanned Aerial Vehicles is introduced in this paper. Networked hierarchical distributed control system is being proposed and its hardware and software structure is briefly described. Mathematical model of a small rotorcraft is ..."
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Abstract — An open project, dealing with autopilot design for autonomous Unmanned Aerial Vehicles is introduced in this paper. Networked hierarchical distributed control system is being proposed and its hardware and software structure is briefly described. Mathematical model of a small rotorcraft
Control system design for rotorcraft-based unmanned aerial vehicles using time-domain system identification
- In IEEE International Conference on Control Applications
, 2000
"... This paper introduces the development of flight control system for rotorcraft-based unmanned aerial vehicle(RUAV). In this research, the linear time-invariant model valid for hover is sought. The system response data is acquired in carefully devised experiment procedure and then a linear time-invari ..."
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Cited by 19 (3 self)
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This paper introduces the development of flight control system for rotorcraft-based unmanned aerial vehicle(RUAV). In this research, the linear time-invariant model valid for hover is sought. The system response data is acquired in carefully devised experiment procedure and then a linear time
American Institute of Aeronautics and Astronautics 1 Blackbird Unmanned Aircraft System
"... The Blackbird Unmanned Aerial System (UAS) has been developed using a systems design approach. The system is defined to include the air vehicle, payload, flight controller, ground station, communications equipment, software and human operators. Design decisions were made based on total system design ..."
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The Blackbird Unmanned Aerial System (UAS) has been developed using a systems design approach. The system is defined to include the air vehicle, payload, flight controller, ground station, communications equipment, software and human operators. Design decisions were made based on total system
Design of an optimal flight control system with integral augmented compensator for a nonlinear UAV helicopter
- Proc. World Congr. Intell. Contr. Auto
"... Abstract—This paper presents the development of an optimal flight control system for a small-scale Unmanned Aerial Vehicle (UAV) helicopter. Complex and highly coupled dynamics of the helicopter naturally complicates the modeling process and the controller design. In this work, the comprehensive non ..."
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Cited by 1 (1 self)
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Abstract—This paper presents the development of an optimal flight control system for a small-scale Unmanned Aerial Vehicle (UAV) helicopter. Complex and highly coupled dynamics of the helicopter naturally complicates the modeling process and the controller design. In this work, the comprehensive
Real-Time System Identification of a Small Multi-Engine Aircraft
"... In-flight identification of an aircraft’s dynamic model can benefit adaptive control schemes by providing estimates of aerodynamic stability derivatives in real time. This information is useful when the dynamic model changes severely in flight such as when faults and failures occur. Moreover a conti ..."
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Cited by 1 (1 self)
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continuously updating model of the aircraft dynamics can be used to monitor the performance of onboard controllers. Flight test data was collected using a sum of sines input implemented in closed loop on a twin engine, fixed wing, Unmanned Aerial Vehicle. This data has been used to estimate a complete six
DETC2009/MESA-87574 FRACTIONAL ORDER FLIGHT CONTROL OF A SMALL FIXED-WING UAV: CONTROLLER DESIGN AND SIMULATION STUDY
"... This paper focuses on designing and implementation of frac-tional order proportional integral (PIα) flight controller on a small fixed-wing unmanned aerial vehicle (UAV). It describes mainly the controller design and simulation studies. The basics of UAV flight control are introduced first with a sp ..."
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This paper focuses on designing and implementation of frac-tional order proportional integral (PIα) flight controller on a small fixed-wing unmanned aerial vehicle (UAV). It describes mainly the controller design and simulation studies. The basics of UAV flight control are introduced first with a
JOURNAL OF AIRCRAFT Vol. 47, No. 4, July–August 2010 Pitch and Heave Control of Robotic Samara Micro Air Vehicles
"... Micro/nano unmanned aerial systems are an emerging class of vehicles uniquely suited to performing covert missions. A linear model for the heave dynamics of a robotic samara (winged seed) in hovering flight was identified from data collected external to the vehicle by a visual tracking system. Insig ..."
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Micro/nano unmanned aerial systems are an emerging class of vehicles uniquely suited to performing covert missions. A linear model for the heave dynamics of a robotic samara (winged seed) in hovering flight was identified from data collected external to the vehicle by a visual tracking system
Cooperative Communication Failure Detection for Multiple Vehicle Systems
"... . For such network of interacting subsystems, some degrees of cooperation for diagnosing the possible failures have shown superior security and reliability rather than using non-cooperative approaches. For example, in Ref. 4, a cooperative fault-detection mechanism is proposed for detecting failure ..."
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is presented for a team of Unmanned Aerial Vehicles (UAV). In order to increase the reliability of sensor fault detection and identification, the method benefits from the capabilities that the team of UAVs offers, by using the additional data from sensors of other UAVs. Furthermore, in Ref. American Institute
System Identification of Small UAVs with MEMS-based Avionics
"... A new MEMS-based small, light, and cost-effective avionics is proposed in order to improve the current situation of system identification of small unmanned aerial vehicles (UAVs), which mostly depends on difficult wind tunnel tests. The avionics is capable of gathering navigation, wind, and control ..."
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A new MEMS-based small, light, and cost-effective avionics is proposed in order to improve the current situation of system identification of small unmanned aerial vehicles (UAVs), which mostly depends on difficult wind tunnel tests. The avionics is capable of gathering navigation, wind, and control
Scaling-up Human Control for Large UAV Teams
, 2006
"... Introduction Wide Area Search Munitions (WASMs) are a cross between an unmanned aerial vehicle and a munition. With an impressive array of onboard sensors and autonomous flight capabilities WASMs might play a variety of roles on the modern battle field including reconnaissance, search, battle damag ..."
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Introduction Wide Area Search Munitions (WASMs) are a cross between an unmanned aerial vehicle and a munition. With an impressive array of onboard sensors and autonomous flight capabilities WASMs might play a variety of roles on the modern battle field including reconnaissance, search, battle
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