Investigation of a Three-Degree Decelerating Approach of a Twin-Engined Jet Aircraft under Actual Flight Conditions-Reference-Cited by-同舟云学术

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Investigation of a Three-Degree Decelerating Approach of a Twin-Engined Jet Aircraft under Actual Flight Conditions

Published:2005-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
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Author:

Schippers Kristof¹,De Prins Johan¹,Mulder Max¹,van Paassen M¹,in 't Veld Alexander¹,Clarke John-Paul²

Affiliation:

1. Delft University of Technology

2. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6139

Reference23 articles.

1. 1Erkelens, L. J. J. "Research on Noise Abatement Procedures," Technical Report NLR-TP-98066, National Aerospace Laboratory, Amsterdam, The Netherlands, 1998.

2. Research into new noise abatement procedures for the 21st century

3. Advanced Noise Abatement Procedures: An Experimental Study of Flight Operational Acceptability

Cited by 3 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. Conceptual Development of the Free-Degree Decelerating Approach;AIAA Guidance, Navigation, and Control Conference;2009-06-14

2. Design of a Pilot Support System to Implement Time-Based Spacing for Decelerating Approaches;AIAA Guidance, Navigation, and Control Conference and Exhibit;2005-06-19

3. Enhanced Self-Spacing Algorithm for Three-Degree Decelerating Approaches;AIAA Guidance, Navigation, and Control Conference and Exhibit;2005-06-19

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