Intelligent FDI system for an aircraft execution element
ICAI'08 Proceedings of the 9th WSEAS International Conference on International Conference on Automation and Information
Programming of a machining procedure for adaptive spiral cutting trajectories
ACMOS'08 Proceedings of the 10th WSEAS International Conference on Automatic Control, Modelling & Simulation
Synthesis of attitude motion of variable mass coaxial bodies
WSEAS Transactions on Systems and Control
Observability of 4th order dynamical systems
SMO'08 Proceedings of the 8th conference on Simulation, modelling and optimization
Lateral control for an aircraft of folding wing
SMO'08 Proceedings of the 8th conference on Simulation, modelling and optimization
High accurate positioning technique for AUV
WSEAS Transactions on Systems and Control
Rezoning techniques for arbitrary Lagrangian-Eulerian computations
CONTROL'08 Proceedings of the 4th WSEAS/IASME international conference on Dynamical systems and control
Nonparametric estimation for control engineering
CONTROL'08 Proceedings of the 4th WSEAS/IASME international conference on Dynamical systems and control
Dynamic stability of the UAV formations fly
SMO'09 Proceedings of the 9th WSEAS international conference on Simulation, modelling and optimization
Stability and control of the UAV formations flight
WSEAS Transactions on Systems and Control
Combat vehicle vibrations during fire in burst
MMES'10 Proceedings of the 2010 international conference on Mathematical models for engineering science
Aircrafts' control and command using hierarchical dynamic inversion
WSEAS Transactions on Systems and Control
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The purpose of this paper is to describe the flight of an Unmanned Aerial Vehicles (UAV) formation by using a 6 degrees of freedom (6 DOF) models. The problem of flight formation will be approached in a simple manner, by using a 3 DOF models, as well as using the complex equations that describe the movement of the 6 DOF for UAV. This theoretical development allows us to define a control structure based on direct commands, which is useful in practical applications. The work will present and analyze the calculus results for each developed solution. The novelty of this paper consists in the definition and testing of some practical solutions for an algorithm that can control an UAV formation. This algorithm allows decrypting the flight of a single UAV, as well as the entire formation. The conclusions will focus the practical possibility of implementing such algorithm on a UAV formation.