• DocumentCode
    3532322
  • Title

    Attitude determination from single camera vector observations

  • Author

    Sazdovski, Vasko ; Silson, Peter M G ; Tsourdos, Antonios

  • Author_Institution
    Dept. of Inf. & Sensors, Cranfield Univ., Swindon, UK
  • fYear
    2010
  • fDate
    7-9 July 2010
  • Firstpage
    49
  • Lastpage
    54
  • Abstract
    Attitude determination is of major importance in Guidance and Control Systems of the Unmanned Aerial Vehicles (UAV´s). Supplying wrong or not precise attitude very often turns to be catastrophic for the UAV´s. Vision sensors are must nowadays. They provide reach source of information given as relative measurements between the vehicle navigation parameters (position, velocity and attitude) and the environment. This paper presents a framework for attitude determination from single camera vector observations. We assume known environment in a form of a map and true vehicle positions from which each observation has been taken. Two different methods for attitude determination are presented: an iterative numerical solution based on Gauss Newton´s method and an exact method known as the Davenport q-method. Pros and cons of the both solutions are presented.
  • Keywords
    Gaussian processes; Newton method; aircraft; aircraft navigation; attitude control; image sensors; remotely operated vehicles; Davenport q-method; Gauss Newton method; attitude determination; iterative numerical solution; single camera vector observations; unmanned aerial vehicles; vehicle navigation parameters; vision sensors; Cameras; Control systems; Gaussian processes; Information resources; Iterative methods; Navigation; Newton method; Position measurement; Unmanned aerial vehicles; Velocity measurement; Davenport q-method; Gauss Newton´s method; attitide; quaternions; single camera; vector observations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Systems (IS), 2010 5th IEEE International Conference
  • Conference_Location
    London
  • Print_ISBN
    978-1-4244-5163-0
  • Electronic_ISBN
    978-1-4244-5164-7
  • Type

    conf

  • DOI
    10.1109/IS.2010.5548331
  • Filename
    5548331