New Sliding Mode Attitude Controller Design Based on Lumped Disturbance Bound Equation-Reference-Cited by-同舟云学术

New Sliding Mode Attitude Controller Design Based on Lumped Disturbance Bound Equation

Published:2018-01 Issue:1 Volume:31 Page:04017082
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sofyalı A.¹,Jafarov E. M.²

Affiliation:

1. Control System Design Engineer, EDS Aerospace, ARI-1 Teknokent, Istanbul Technical Univ., Ayazaga Campus, Maslak, Sariyer, Istanbul 34469, Turkey (corresponding author).

2. Professor, Faculty of Aeronautics and Astronautics, Dept. of Aeronautical Engineering, Istanbul Technical Univ., Ayazaga Campus, Maslak, Sariyer, Istanbul 34469, Turkey.

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.1943-5525.0000791

Reference30 articles.

1. Bak T. (1999). “Spacecraft attitude determination: A magnetometer approach.” Ph.D. thesis Aalborg Univ. Aalborg Denmark.

2. CelesTrak. (2015). “NORAD two-line element sets.” ⟨http://celestrak.com/NORAD/elements/⟩ (May 2 2015).

3. Sliding-mode controller design for spacecraft attitude tracking maneuvers;Chen Y. P.;IEEE Trans. Aerospace Electronic Syst.,1993

4. A robust attitude control strategy with guaranteed transient performance via modified Lyapunov-based control and integral sliding mode control;Chen Z.;Nonlinear Dyn.,2014

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