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Research Article | Open Access
Volume 2 | Issue 8 | Year 2015 | Article Id. IJECE-V2I8P107 | DOI : https://doi.org/10.14445/23488549/IJECE-V2I8P107

Simulation of 6-DOF

B.Navya, V.JyothiSri and B.Shilpa

Citation :

B.Navya, V.JyothiSri and B.Shilpa, "Simulation of 6-DOF," International Journal of Electronics and Communication Engineering, vol. 2, no. 8, pp. 16-20, 2015. Crossref, https://doi.org/10.14445/23488549/IJECE-V2I8P107

Abstract

 6-DOF (Degrees of Freedom) is intended for simulation of Aerospace Vehicle dynamics and kinematics for testing and validating of Guidance, Navigation and Control. It is used to simulate all the three Translational and Rotational axes of the vehicle (The system is interfaced with MIU, INS and OBC).This system is useful for verification and validation of On-Board Computer Software. In aerospace vehicle, simulation S/W is the complete Model of the Plant and Algorithm (Navigation, Guidance, Control and Mission Sequence).This Model gives body rates and accelerations by 6DOF equations. Its inputs are thrust and control deflections. Forces and Moments are generated using Aerodynamic Force Coefficients and Moment Coefficients given by Aerodynamic Division.

Keywords

6 degrees of freedom, Reaction control system, Fuel nozzle controller.

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