Optimal trajectory generation of launch vehicle using PSO algorithm

M. V. Dileep; Surekha Kamath; Vishnu G. Nair

doi:10.1109/ABLAZE.2015.7154970

Optimal trajectory generation of launch vehicle using PSO algorithm

M. V. Dileep, Surekha Kamath, Vishnu G. Nair

Manipal Institute of Technology, Manipal

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

3 Citations (Scopus)

Abstract

This paper presents an approach to solve a trajectory optimization problem for a launch vehicle using particle swarm optimization. Trajectory generation for a single stage liquid propellant launch vehicle is considered by using angle of attack as a control variable. The problem is solved by considering minimization of terminal error as an objective with some path constraints and fixed boundary conditions. The burning time of the liquid rocket engine is fixed, leading to fixed time problem. Two different types of inertia weight is examined in this problem, one is the random function and the other is linearly varying. The effectiveness is verified using simulation results obtained from Matlab simulation environment.

Original language	English
Title of host publication	2015 1st International Conference on Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	56-60
Number of pages	5
ISBN (Electronic)	9781479984336
DOIs	https://doi.org/10.1109/ABLAZE.2015.7154970
Publication status	Published - 10-07-2015
Event	2015 1st International Conference On Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015 - Greater Noida, India Duration: 25-02-2015 → 27-02-2015

Conference

Conference	2015 1st International Conference On Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015
Country/Territory	India
City	Greater Noida
Period	25-02-15 → 27-02-15

All Science Journal Classification (ASJC) codes

Computer Networks and Communications
Information Systems
Signal Processing
Computational Theory and Mathematics

Access to Document

10.1109/ABLAZE.2015.7154970

Cite this

@inproceedings{0ebc9ce13d3044208ceda23d1b94bc25,

title = "Optimal trajectory generation of launch vehicle using PSO algorithm",

abstract = "This paper presents an approach to solve a trajectory optimization problem for a launch vehicle using particle swarm optimization. Trajectory generation for a single stage liquid propellant launch vehicle is considered by using angle of attack as a control variable. The problem is solved by considering minimization of terminal error as an objective with some path constraints and fixed boundary conditions. The burning time of the liquid rocket engine is fixed, leading to fixed time problem. Two different types of inertia weight is examined in this problem, one is the random function and the other is linearly varying. The effectiveness is verified using simulation results obtained from Matlab simulation environment.",

author = "Dileep, {M. V.} and Surekha Kamath and Nair, {Vishnu G.}",

year = "2015",

month = jul,

day = "10",

doi = "10.1109/ABLAZE.2015.7154970",

language = "English",

pages = "56--60",

booktitle = "2015 1st International Conference on Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

address = "United States",

note = "2015 1st International Conference On Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015 ; Conference date: 25-02-2015 Through 27-02-2015",

}

Dileep, MV, Kamath, S & Nair, VG 2015, Optimal trajectory generation of launch vehicle using PSO algorithm. in 2015 1st International Conference on Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015., 7154970, Institute of Electrical and Electronics Engineers Inc., pp. 56-60, 2015 1st International Conference On Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015, Greater Noida, India, 25-02-15. https://doi.org/10.1109/ABLAZE.2015.7154970

Optimal trajectory generation of launch vehicle using PSO algorithm. / Dileep, M. V.; Kamath, Surekha ; Nair, Vishnu G.
2015 1st International Conference on Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015. Institute of Electrical and Electronics Engineers Inc., 2015. p. 56-60 7154970.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

TY - GEN

T1 - Optimal trajectory generation of launch vehicle using PSO algorithm

AU - Dileep, M. V.

AU - Kamath, Surekha

AU - Nair, Vishnu G.

PY - 2015/7/10

Y1 - 2015/7/10

N2 - This paper presents an approach to solve a trajectory optimization problem for a launch vehicle using particle swarm optimization. Trajectory generation for a single stage liquid propellant launch vehicle is considered by using angle of attack as a control variable. The problem is solved by considering minimization of terminal error as an objective with some path constraints and fixed boundary conditions. The burning time of the liquid rocket engine is fixed, leading to fixed time problem. Two different types of inertia weight is examined in this problem, one is the random function and the other is linearly varying. The effectiveness is verified using simulation results obtained from Matlab simulation environment.

AB - This paper presents an approach to solve a trajectory optimization problem for a launch vehicle using particle swarm optimization. Trajectory generation for a single stage liquid propellant launch vehicle is considered by using angle of attack as a control variable. The problem is solved by considering minimization of terminal error as an objective with some path constraints and fixed boundary conditions. The burning time of the liquid rocket engine is fixed, leading to fixed time problem. Two different types of inertia weight is examined in this problem, one is the random function and the other is linearly varying. The effectiveness is verified using simulation results obtained from Matlab simulation environment.

UR - http://www.scopus.com/inward/record.url?scp=84941237057&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84941237057&partnerID=8YFLogxK

U2 - 10.1109/ABLAZE.2015.7154970

DO - 10.1109/ABLAZE.2015.7154970

M3 - Conference contribution

AN - SCOPUS:84941237057

SP - 56

EP - 60

BT - 2015 1st International Conference on Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2015 1st International Conference On Futuristic Trends in Computational Analysis and Knowledge Management, ABLAZE 2015

Y2 - 25 February 2015 through 27 February 2015

ER -

Optimal trajectory generation of launch vehicle using PSO algorithm

Abstract

Conference

All Science Journal Classification (ASJC) codes

Access to Document

Other files and links

Fingerprint

Cite this