Numerical Simulation of Rocket Launch Vehicle

8 Pages Posted: 23 Dec 2019

See all articles by Dhanush G J,

Dhanush G J,

S J C Institute of Technology

Manju Nath

S J C Institute of Technology

Deepak B S,

S J C Institute of Technology

Deepa M S

S. J. C. I. T, Chickballapur

Ajith Patil J R

S J C Institute of Technology

Date Written: May 17, 2019

Abstract

Launching of Rocket is a complex phenomenon. There is high chance of failure in such missions. Hence it is necessary to predict the launch path or Trajectory, External disturbances and various other parameters. Numerical Simulation is one such way of predicting launch parameters which helps in taking precautions preventing failure. This Paper presents a platform for simulation of Rocket launch vehicle and control Law validation. The analysis is performed during the Lift-off phase in atmosphere using a mathematical nonlinear dynamic model. Set of six degrees of freedom equations of motion with necessary reference frames and transformations in between them is developed. The Mathematical Model is applied in MATLAB and Simulink simulation which can be easily adjusted for any type of launch vehicle or rocket.

Keywords: Simulation of Rocket Launch Vehicle, Mathematical model, Numerical Simulation, Six degree of freedom equation of motion

Suggested Citation

G J,, Dhanush and Nath, Manju and B S,, Deepak and M S, Deepa and Patil J R, Ajith, Numerical Simulation of Rocket Launch Vehicle (May 17, 2019). Available at SSRN: https://ssrn.com/abstract=3507916 or http://dx.doi.org/10.2139/ssrn.3507916

Dhanush G J, (Contact Author)

S J C Institute of Technology ( email )

B.B. Road
Chikkaballapur, 562 101
India

Manju Nath

S J C Institute of Technology ( email )

B.B. Road
Chikkaballapur, 562 101
India

Deepak B S,

S J C Institute of Technology ( email )

B.B. Road
Chikkaballapur, 562 101
India

Deepa M S

S. J. C. I. T, Chickballapur ( email )

Chickballapur
India

Ajith Patil J R

S J C Institute of Technology ( email )

B.B. Road
Chikkaballapur, 562 101
India

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