Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method

The particle swarm-based micro air launch vehicle trajectory optimization method is carried out by formulating a parameter optimization problem, which is solved using a particle swarm optimization procedure. The optimization problem is formulated using a single objective function having the exp...

Full description

Bibliographic Details
Main Authors: Omar, Hanafy, Idres, Moumen, Kafafy, Raed
Format: Patent
Language:English
Published: 2012
Subjects:
Online Access:http://irep.iium.edu.my/43938/
http://irep.iium.edu.my/43938/1/Patent-Particle_Swarm-Based_Micro_Air_Launch_Vehicle_Trajectory_Optimization_Method-US20120053764A1.pdf
_version_ 1848782527017254912
author Omar, Hanafy
Idres, Moumen
Kafafy, Raed
author_facet Omar, Hanafy
Idres, Moumen
Kafafy, Raed
author_sort Omar, Hanafy
building IIUM Repository
collection Online Access
description The particle swarm-based micro air launch vehicle trajectory optimization method is carried out by formulating a parameter optimization problem, which is solved using a particle swarm optimization procedure. The optimization problem is formulated using a single objective function having the explicit objective to maximize the payload mass. Constraints on terminal conditions are imposed.
first_indexed 2025-11-14T16:06:52Z
format Patent
id iium-43938
institution International Islamic University Malaysia
institution_category Local University
language English
last_indexed 2025-11-14T16:06:52Z
publishDate 2012
recordtype eprints
repository_type Digital Repository
spelling iium-439382015-07-21T06:38:13Z http://irep.iium.edu.my/43938/ Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method Omar, Hanafy Idres, Moumen Kafafy, Raed TJ Mechanical engineering and machinery The particle swarm-based micro air launch vehicle trajectory optimization method is carried out by formulating a parameter optimization problem, which is solved using a particle swarm optimization procedure. The optimization problem is formulated using a single objective function having the explicit objective to maximize the payload mass. Constraints on terminal conditions are imposed. 2012-03-01 Patent NonPeerReviewed application/pdf en http://irep.iium.edu.my/43938/1/Patent-Particle_Swarm-Based_Micro_Air_Launch_Vehicle_Trajectory_Optimization_Method-US20120053764A1.pdf Omar, Hanafy and Idres, Moumen and Kafafy, Raed (2012) Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method. http://www.google.com/patents/US8332085. http://patft.uspto.gov/netahtml/PTO/srchnum.htm http://www.google.com/patents/US8332085
spellingShingle TJ Mechanical engineering and machinery
Omar, Hanafy
Idres, Moumen
Kafafy, Raed
Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method
title Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method
title_full Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method
title_fullStr Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method
title_full_unstemmed Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method
title_short Particle Swarm-Based Micro Air Launch Vehicle Trajectory Optimization Method
title_sort particle swarm-based micro air launch vehicle trajectory optimization method
topic TJ Mechanical engineering and machinery
url http://irep.iium.edu.my/43938/
http://irep.iium.edu.my/43938/
http://irep.iium.edu.my/43938/
http://irep.iium.edu.my/43938/1/Patent-Particle_Swarm-Based_Micro_Air_Launch_Vehicle_Trajectory_Optimization_Method-US20120053764A1.pdf