Day 1, April 14 - Posters

Title

Mathematical modeling of variable mass rocket’s dynamics using the differential transform method

Start Date

14-4-2020 9:00 AM

End Date

14-4-2020 11:00 AM

Publisher

University of Tennessee at Chattanooga

Place of Publication

Chattanooga (Tenn.)

Abstract

The Riccati Differential Equation that defines a rocket's velocity as a function of time is semi-analytically solved using the Differential Transform Method to simulate a rocket's flight.

Date

April 2020

Document Type

posters

Language

English

Rights

http://rightsstatement.org/vocab/InC/1.0/

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Apr 14th, 9:00 AM Apr 14th, 11:00 AM

Mathematical modeling of variable mass rocket’s dynamics using the differential transform method

The Riccati Differential Equation that defines a rocket's velocity as a function of time is semi-analytically solved using the Differential Transform Method to simulate a rocket's flight.