Autopilot Supported by Nonlinear Model Following Reconfigurable Flight Control System-Reference-Cited by-同舟云学术

Autopilot Supported by Nonlinear Model Following Reconfigurable Flight Control System

Published:2010-10 Issue:4 Volume:23 Page:339-347
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zugaj M.¹²,Narkiewicz J.¹²

Affiliation:

1. Associate Professor, Institute of Aeronautics and Applied Mechanics, Warsaw Univ. of Technology, ul. Nowowiejska 24, 00-665 Warszawa, Poland (corresponding author).

2. Professor, Institute of Aeronautics and Applied Mechanics, Warsaw Univ. of Technology, ul. Nowowiejska 24, 00-665 Warszawa, Poland.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000050

Reference11 articles.

1. Reconfigurable Nonlinear Autopilot

2. Landing safely when flight controls fail;Burcham B.;Aerosp. Am.,1997

3. Two Reconfigurable Flight-Control Design Methods: Robust Servomechanism and Control Allocation

4. Development of a Reconfigurable Flight Control Law for Tailless Aircraft

5. Sliding Mode Control Applied to Reconfigurable Flight Control Design

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