Linearized State-Space Model-Based Attitude Control for Rocket With Four Controllable Fins—Part 1-1: Basic Modeling and Identification
Author:
Affiliation:
1. Faculty of Smart Vehicle System Engineering, Chosun University, Dong-gu, South Korea
2. Department of Smart Air Mobility, Korea Aerospace University, Deogyang-gu, South Korea
Funder
Gwangju Green Environment Center as “Research Development Project” in 2022
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
General Engineering,General Materials Science,General Computer Science,Electrical and Electronic Engineering
Link
http://xplorestaging.ieee.org/ielx7/6287639/10005208/10336811.pdf?arnumber=10336811
Reference29 articles.
1. Finite-Horizon Near-Optimal Approach and Landing Planning of Reusable Launch Vehicles
2. An adaptive optimization algorithm based on clustering analysis for return multi-flight-phase of VTVL reusable launch vehicle
3. Trajectory Planning and Soft Landing of RLV Using Non-Linear Model Predictive Control
4. Wind tunnel experiments of interstage segments used for aerodynamic control of retro-propulsion assisted landing vehicles
5. Online Trajectory Optimization Method for Large Attitude Flip Vertical Landing of Starship-like Vehicles
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