Retrospective Cost Adaptive Control of Unstart in a Model Scramjet Combustor-Reference-Cited by-同舟云学术

Retrospective Cost Adaptive Control of Unstart in a Model Scramjet Combustor

Published:2018-03 Issue:3 Volume:56 Page:1085-1096
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Goel Ankit¹,Duraisamy Karthik¹,Bernstein Dennis S.¹

Affiliation:

1. University of Michigan, Ann Arbor, Michigan 48109

Funder

National Science Foundation

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J055812

Reference21 articles.

1. Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment

2. Robust Control for Unstart Recovery in Hypersonic Vehicles

3. HutzelJ. R. “Scramjet Isolator Modeling and Control,” ProQuest Dissertations Publ. U.S. Air Force Inst. of Technology Rept. AFIT/DS/ENY/11-19, Wright-Patterson AFB, OH, 2011.

4. Ascent Trajectories of Hypersonic Aircraft: Operability Limits Due to Engine Unstart

5. A Numerical Study of Filtering and Control for Scramjet Engine Flow

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