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
Link To Document :
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