Conceptual Study on Control-Integrated Design Based on Multidisciplinary Tradeoff Needs for Morphing Waveriders-Reference-Cited by-同舟云学术

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Conceptual Study on Control-Integrated Design Based on Multidisciplinary Tradeoff Needs for Morphing Waveriders

Published:2014-07 Issue:4 Volume:27 Page:04014008
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Yanbin¹,Xiao Dibo²,Zhang Yong³,Lu Yuping⁴

Affiliation:

1. Associate Professor, College of Astronautics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China (corresponding author).

2. Ph.D. Candidate, College of Astronautics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

3. Researcher, College of Astronautics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

4. Professor, College of Astronautics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

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.1943-5525.0000392

Reference38 articles.

1. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle

2. Bye D. R. and McClure P. D. (2007). “Design of a morphing vehicle.” Proc. 48th AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conf. American Institute of Aeronautics and Astronautics Reston VA.

3. Analytical aeropropulsive-aeroelastic hypersonic-vehicle model with dynamic analysis

4. Clark A. D. Mirmirani M. D. Wu C. Choi S. and Kuipers M. (2006). “An aero-propulsion integrated elastic model of a generic airbreathing hypersonic vehicle.” Proc. AIAA Guidance Navigation and Control Conf. and Exhibit American Institute of Aeronautics and Astronautics Reston VA.

5. Nonlinear Ten-Degree-of-Freedom Dynamics Model of a Generic Hypersonic Vehicle

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