An optimal soft landing control for moon lander by means of measures

J. A. Fakharzadeh; Sahar Salehi

doi:10.4028/www.scientific.net/AMM.52-54.1861

An optimal soft landing control for moon lander by means of measures

J. A. Fakharzadeh, Sahar Salehi

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

Abstract

Designing a new control strategy for a moon lander to achieve an optimal soft landing, is the main purpose of this paper. For the dynamical system of the propeller to achieve the lowest level of fuel consumption, the problem of soft landing is presented as an optimal control one. Representing this into a variational form, transferring to an optimization problem on a measure space and then determining the optimal solution via a linear programming problem is the new solution path. This method has some important advantages in compare with the other, which are explain within a numerical simulation.

Original language	English
Title of host publication	Advances in Mechanical Engineering
Pages	1861-1867
Number of pages	7
DOIs	https://doi.org/10.4028/www.scientific.net/AMM.52-54.1861
Publication status	Published - 2011
Event	2011 1st International Conference on Mechanical Engineering, ICME 2011 - Phuket, Thailand Duration: 2011 Apr 3 → 2011 Apr 4

Publication series

Name	Applied Mechanics and Materials
Volume	52-54
ISSN (Print)	1660-9336
ISSN (Electronic)	1662-7482

Other

Other	2011 1st International Conference on Mechanical Engineering, ICME 2011
Country/Territory	Thailand
City	Phuket
Period	11/4/3 → 11/4/4

Keywords

LP
Measure
Moon lander
Optimal control
Soft landing

ASJC Scopus subject areas

Engineering(all)

Access to Document

10.4028/www.scientific.net/AMM.52-54.1861

Cite this

@inproceedings{17739491b79040b68650da346d8a66f9,

title = "An optimal soft landing control for moon lander by means of measures",

abstract = "Designing a new control strategy for a moon lander to achieve an optimal soft landing, is the main purpose of this paper. For the dynamical system of the propeller to achieve the lowest level of fuel consumption, the problem of soft landing is presented as an optimal control one. Representing this into a variational form, transferring to an optimization problem on a measure space and then determining the optimal solution via a linear programming problem is the new solution path. This method has some important advantages in compare with the other, which are explain within a numerical simulation.",

keywords = "LP, Measure, Moon lander, Optimal control, Soft landing",

author = "Fakharzadeh, {J. A.} and Sahar Salehi",

year = "2011",

doi = "10.4028/www.scientific.net/AMM.52-54.1861",

language = "English",

isbn = "9783037850770",

series = "Applied Mechanics and Materials",

pages = "1861--1867",

booktitle = "Advances in Mechanical Engineering",

}

TY - GEN

T1 - An optimal soft landing control for moon lander by means of measures

AU - Fakharzadeh, J. A.

AU - Salehi, Sahar

PY - 2011

Y1 - 2011

N2 - Designing a new control strategy for a moon lander to achieve an optimal soft landing, is the main purpose of this paper. For the dynamical system of the propeller to achieve the lowest level of fuel consumption, the problem of soft landing is presented as an optimal control one. Representing this into a variational form, transferring to an optimization problem on a measure space and then determining the optimal solution via a linear programming problem is the new solution path. This method has some important advantages in compare with the other, which are explain within a numerical simulation.

AB - Designing a new control strategy for a moon lander to achieve an optimal soft landing, is the main purpose of this paper. For the dynamical system of the propeller to achieve the lowest level of fuel consumption, the problem of soft landing is presented as an optimal control one. Representing this into a variational form, transferring to an optimization problem on a measure space and then determining the optimal solution via a linear programming problem is the new solution path. This method has some important advantages in compare with the other, which are explain within a numerical simulation.

KW - LP

KW - Measure

KW - Moon lander

KW - Optimal control

KW - Soft landing

UR - http://www.scopus.com/inward/record.url?scp=79954497757&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=79954497757&partnerID=8YFLogxK

U2 - 10.4028/www.scientific.net/AMM.52-54.1861

DO - 10.4028/www.scientific.net/AMM.52-54.1861

M3 - Conference contribution

AN - SCOPUS:79954497757

SN - 9783037850770

T3 - Applied Mechanics and Materials

SP - 1861

EP - 1867

BT - Advances in Mechanical Engineering

T2 - 2011 1st International Conference on Mechanical Engineering, ICME 2011

Y2 - 3 April 2011 through 4 April 2011

ER -

An optimal soft landing control for moon lander by means of measures

Abstract

Publication series

Other

Keywords

ASJC Scopus subject areas

Access to Document

Other files and links

Fingerprint

Cite this