Linearized State-Space Model-Based Attitude Control for Rocket With Four Controllable Fins—Part 1-1: Basic Modeling and Identification

Linearized State-Space Model-Based Attitude Control for Rocket With Four Controllable Fins—Part 1-1: Basic Modeling and Identification

In this study, we present, analyze, and validate a linear state-space model for a simplified rocket with four fins. The model is validated experimentally using a wind tunnel. The proposed model consists of two main elements: a rocket body and fins. The body is represented as a cylinder integrated fr...

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Bibliographic Details
Main Authors: Shinhyung Kim, Abera Tullu, Sunghun Jung
Format: Article
Language:English
Published: IEEE 2023-01-01
Series:IEEE Access
Subjects:
Flight test system
hardware-in-the-loop simulation
model validation
rocket
software-in-the-loop simulation
state-space model
Online Access:https://ieeexplore.ieee.org/document/10336811/

Internet

https://ieeexplore.ieee.org/document/10336811/

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