@inproceedings{AliMontenegro2015,
  author    = {Ali, Qasim and Montenegro, Sergio},
  title     = {A Simple Approach to Quadrocopter Formation Flying Test Setup for Education and Development},
  series = {INTED2015 Proceedings},
  booktitle = {INTED2015 Proceedings},
  publisher = {International Academy of Technology, Education and Development (IATED)},
  isbn      = {978-84-606-5763-7},
  issn      = {2340-1079},
  url       = {http://nbn-resolving.de/urn:nbn:de:bvb:20-opus-114495},
  pages     = {2776 -- 2784},
  year      = {2015},
  abstract  = {A simple test setup has been developed at Institute of Aerospace Information Technology, University of W{\"u}rzburg, Germany to realize basic functionalities for formation flight of quadrocopters. The test environment is planned to be utilized for developing and validating the algorithms for formation flying capability in real environment as well as for education purpose. An already existing test bed for single quadrocopter was extended with necessary inter-communication and distributed control mechanism to test the algorithms for formation flights in 2 degrees of freedom (roll / pitch). This study encompasses the domain of communication, control engineering and embedded systems programming. Bluetooth protocol has been used for inter-communication between two quadrocopters. A simple approach of PID control in combination with Kalman filter has been exploited. MATLAB Instrument Control Toolbox has been used for data display, plotting and analysis. Plots can be drawn in real-time and received information can also be stored in the form of files for later use and analysis. The test setup has been developed indigenously and at considerably low cost. Emphasis has been placed on simplicity to facilitate students learning process. Several lessons have been learnt during the course of development of this setup. Proposed setup is quite flexible that can be modified as per changing requirements.},
  subject      = {Flugk{\"o}rper},
  language  = {en}
}
@article{GageikStrohmeierMontenegro2013,
  author    = {Gageik, Nils and Strohmeier, Michael and Montenegro, Sergio},
  title     = {Waypoint flight parameter comparison of an autonomous UAV},
  series = {International Journal of Artificial Intelligence \& Applications (IJAIA)},
  journal   = {International Journal of Artificial Intelligence \& Applications (IJAIA)},
  doi       = {10.5121/ijaia.2013.4304},
  url       = {http://nbn-resolving.de/urn:nbn:de:bvb:20-opus-96833},
  year      = {2013},
  abstract  = {The present paper compares the effect of different waypoint parameters on the flight performance of a special autonomous indoor UAV (unmanned aerial vehicle) fusing ultrasonic, inertial, pressure and optical sensors for 3D positioning and controlling. The investigated parameters are the acceptance threshold for reaching a waypoint as well as the maximal waypoint step size or block size. The effect of these parameters on the flight time and accuracy of the flight path is investigated. Therefore the paper addresses how the acceptance threshold and step size influence the speed and accuracy of the autonomous flight and thus influence the performance of the presented autonomous quadrocopter under real indoor navigation circumstances. Furthermore the paper demonstrates a drawback of the standard potential field method for navigation of such autonomous quadrocopters and points to an improvement.},
  language  = {en}
}
@article{GageikStrohmeierMontenegro2013,
  author    = {Gageik, Nils and Strohmeier, Michael and Montenegro, Sergio},
  title     = {An Autonomous UAV with an Optical Flow Sensor for Positioning and Navigation},
  series = {International Journal of Advanced Robotic Systems},
  journal   = {International Journal of Advanced Robotic Systems},
  doi       = {10.5772/56813},
  url       = {http://nbn-resolving.de/urn:nbn:de:bvb:20-opus-96368},
  year      = {2013},
  abstract  = {A procedure to control all six DOF (degrees of freedom) of a UAV (unmanned aerial vehicle) without an external reference system and to enable fully autonomous flight is presented here. For 2D positioning the principle of optical flow is used. Together with the output of height estimation, fusing ultrasonic, infrared and inertial and pressure sensor data, the 3D position of the UAV can be computed, controlled and steered. All data processing is done on the UAV. An external computer with a pathway planning interface is for commanding purposes only. The presented system is part of the AQopterI8 project, which aims to develop an autonomous flying quadrocopter for indoor application. The focus of this paper is 2D positioning using an optical flow sensor. As a result of the performed evaluation, it can be concluded that for position hold, the standard deviation of the position error is 10cm and after landing the position error is about 30cm.},
  language  = {en}
}