Optimal Tuning of Adaptive Augmenting Controller for Launch Vehicles in Atmospheric Flight-Reference-Cited by-同舟云学术

Optimal Tuning of Adaptive Augmenting Controller for Launch Vehicles in Atmospheric Flight

Published:2020-11 Issue:11 Volume:43 Page:2133-2140
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Trotta Domenico¹,Zavoli Alessandro¹,De Matteis Guido¹,Neri Agostino²

Affiliation:

1. University of Rome “La Sapienza”, 00184 Rome, Italy

2. ESA, I-00044 Frascati, Italy

Funder

European Space Agency

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference13 articles.

1. also American Astronomical Soc. Paper 14-038, San Diego, CA, 2014.

2. Evaluating the stability of NASA’s space launch system with adaptive augmenting control

3. Robust optimization – A comprehensive survey

4. GreensiteA. L. “Analysis and Design of Space Vehicle Flight Control Systems. Volume I-Short Period Dynamics,” NASA CR-820, GD/C-DDE65-055, 1967.

5. GreensiteA. L. “Analysis and Design of Space Vehicle Flight Control Systems. Volume VII-Attitude Control During Launch,” NASA CR-826, GD/C-DDE66-028, 1967.

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