Ascent Trajectory Optimization of Launch Vehicle Using Controlled Random Search-Reference-Cited by-同舟云学术

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Ascent Trajectory Optimization of Launch Vehicle Using Controlled Random Search

Published:2023-05-19 Issue: Volume: Page:
ISSN:
Container-title:2023 International Conference on Control, Communication and Computing (ICCC)
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Author:

Gilson Cindrella¹,A Sabarinath²,S Lal Priya P¹

Affiliation:

1. College of Engineering Trivandrum,Department of Electrical Engineering,Kerala,India

2. Vikram Sarabhai Space Centre,Space Transportation System,Kerala,India

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10164829/10164822/10165455.pdf?arnumber=10165455

Reference11 articles.

1. Swarm, Evolutionary, and Memetic Computing

2. Entry, descent, landing and ascent;avanzini;Lecture Notes-Ver,2009

3. Computational algorithms based on random search for solving global optimization problems

4. Fuzzy Optimal Control Approach in Low-Thrust Orbit Transfer Problem

5. Optimal trajectory generation of launch vehicle using PSO algorithm

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