Model Predictive Control Architecture for Rotorcraft Inverse Simulation-Reference-Cited by-同舟云学术

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Model Predictive Control Architecture for Rotorcraft Inverse Simulation

Published:2013-01 Issue:1 Volume:36 Page:207-217
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Avanzini Giulio¹,Thomson Douglas²,Torasso Alberto³

Affiliation:

1. Department of Engineering, Università del Salento, Lecce 73100, Italy

2. Head of Aerospace Sciences Research Division, University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom

3. Department of Mechanical and Aerospace Engineering, Politecnico di Torino, Turin 10129, Italy

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.56563

Reference23 articles.

1. Inverse simulation as a tool for flight dynamics research—Principles and applications

2. A Generalized Algorithm for Inverse Simulation Applied to Helicopter Maneuvering Flight

3. An interpretation of airplane general motion and contol as inverse problem

4. Generalized technique for inverse simulation applied to aircraft maneuvers

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4. Fault-Tolerant Trajectory Tracking Control of a Quadrotor Suffering a Complete Rotor Failure;2021 33rd Chinese Control and Decision Conference (CCDC);2021-05-22

5. Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model;International Journal of Turbo & Jet-Engines;2020-08-08

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