Reentry Trajectory Design with Pigeon Inspired Optimization Using Derived Angle of Attack Profile-Reference-Cited by-同舟云学术

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Reentry Trajectory Design with Pigeon Inspired Optimization Using Derived Angle of Attack Profile

Published:2018-11 Issue:6 Volume:31 Page:04018104
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sushnigdha Gangireddy¹,Joshi Ashok²

Affiliation:

1. Research Scholar, Dept. of Aerospace Engineering, Indian Institute of Technology Bombay, Mumbai, Maharashtra 400076, India (corresponding author).

2. Professor, Dept. of Aerospace Engineering, Indian Institute of Technology Bombay, Mumbai, Maharashtra 400076, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000929

Reference23 articles.

1. Optimal guidance for reentry vehicles based on indirect legendre pseudospectral method;Bailing T.;Acta Astronaut.,2011

2. Optimal guidance for hypersonic reentry using inversion and receding horizon control

3. Artificial bee colony–based direct collocation for reentry trajectory optimization of hypersonic vehicle

4. Pigeon-inspired optimization: a new swarm intelligence optimizer for air robot path planning

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1. Online Trajectory Replan for Gliding Vehicle Considering Terminal Velocity Constraint;IEEE Transactions on Aerospace and Electronic Systems;2022

2. A novel search space reduction optimization algorithm;Soft Computing;2021-05-07

3. Hypersonic reentry trajectory planning by using hybrid fractional-order particle swarm optimization and gravitational search algorithm;Chinese Journal of Aeronautics;2021-01

4. Reentry guidance by accelerated fractional-order particle swarm optimization method;Aircraft Engineering and Aerospace Technology;2020-07-22

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