Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft-Reference-Cited by-同舟云学术

Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft

Published:1994-08-01 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Garg Sanjay¹,Mattern Duane²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. NYMA, Inc., Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3611

Reference7 articles.

1. VL Controls Integration Program," final report for NASA contract 25194, Pratt & Whitney, West Palm October 1993. [7] Garg, S., Ouzts, P., Lorenzo, C.F., and Mattem, D.L. "IMPAC - an Integrated Methodology for Propulsion and A i h e Control," 1991 American Control Conference, Boston, MA, June I991. [8] Garg, S. "Robust Integrated FlightlPropulsion Control Design fora STOVLAircraftUsingH-Infinity Control Design Techniques,"Automatica, Vol.29,No.

2. Partitioning of centralized integrated flight/propulsion control design for decentralized implementation

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aircraft Turbine Engine Control Research at NASA Glenn Research Center;Journal of Aerospace Engineering;2013-04

2. A partitioned integrated flight and propulsion control system with engine safety limiting;Control Engineering Practice;2000-08

3. Sensor validation for turbofan engines using an autoassociative neural network;Guidance, Navigation, and Control Conference;1996-07-29

4. Piloted evaluation of an integrated methodology for propulsion and airframe control design;Guidance, Navigation, and Control Conference;1994-08-01