A new thrust vector-controlled rocket based on JOA using MCDA

A new thrust vector-controlled rocket based on JOA using MCDA

A thrust vector-controlled rocket model consists of army science board model responsible for computing the angles of the gravity center with a directivity of trajectory positions (x, z). A thrust vector-controlled rocket model is known to be #TVCASB for fall trajectory correction solving, but the fa...

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Bibliographic Details
Main Authors: Noorulden Basil, Hamzah M. Marhoon, Ahmed R. Ibrahim
Format: Article
Language:English
Published: Elsevier 2023-04-01
Series:Measurement: Sensors
Subjects:
Thrust vector-controlled rocket model
Army science board
Jaya optimization algorithm
Multi-criteria decision making
Fractional order proportional integral derivative controller
Online Access:http://www.sciencedirect.com/science/article/pii/S2665917423000089

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http://www.sciencedirect.com/science/article/pii/S2665917423000089

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