Day 1, April 14 - Posters
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/
Recommended Citation
Sam, Ashwyn, "Mathematical modeling of variable mass rocket’s dynamics using the differential transform method". ReSEARCH Dialogues Conference proceedings. https://scholar.utc.edu/research-dialogues/2020/day1_posters/53.
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.