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Attitude Control of Rocket via Thrust Vector Control Technique

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dc.contributor.author BOUHADIBA, SLIMANE
dc.contributor.author BENDJEFAL, ILYAS
dc.date.accessioned 2022-10-23T14:15:19Z
dc.date.available 2022-10-23T14:15:19Z
dc.date.issued 2022-07-06
dc.identifier.uri http://hdl.handle.net/STDB_UNAM/387
dc.description.abstract Rocket control was primarily complex and aimed at one objective which is maintaining flight path directory and an advanced one which is an automotive flight mission flexible to different delivered inputs from communication guidance navigation and changing orbits. Thus, making a control model of rockets will impact industrial sectors in many ways from satellite emplacement to helping researchers internet connection and military purposes; thrust vector control TVC is the general technique of rocket control thus in this thesis we are willing to demonstrate the attitude control of small scaled rocket with linear control and this work will be in 3 chapters. Chapter 1 dedicated for rocket history and the TVC in general. Chapter 2 about the mathematical model for the rocket dynamics and will be on implementing a linear control method for our dynamical model. Chapter 3 will be about experimentation controlling two degree of freedom “pitch and yaw”. en_US
dc.language.iso en en_US
dc.publisher Directeur: Mr. ARICHI Fayssal / Co-Directeur: Mr. MOKHTARI Mohammed Réda en_US
dc.title Attitude Control of Rocket via Thrust Vector Control Technique en_US
dc.type Thesis en_US

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