• DocumentCode
    3398707
  • Title

    Fuel efficient strategies for reducing contrail formations in United States airspace

  • Author

    Sridhar, B. ; Chen, N.Y. ; Ng, H.K.

  • Author_Institution
    Ames Res. Center, NASA, Moffett Field, CA, USA
  • fYear
    2010
  • fDate
    3-7 Oct. 2010
  • Abstract
    This paper describes a class of strategies for reducing persistent contrail formation in the United States airspace. The primary objective is to minimize potential contrail formation regions by altering the aircraft´s cruising altitude in a fuel-efficient way. The results show that the contrail formations can be reduced significantly without extra fuel consumption and without adversely affecting congestion in the airspace. The contrail formations can be further reduced by using extra fuel. For the day tested, the maximal reduction strategy has a 53% contrail reduction rate. The most fuel-efficient strategy has an 8% reduction rate with 2.86% less fuel-burnt compared to the maximal reduction strategy. Using a cost function which penalizes extra fuel consumed while maximizing the amount of contrail reduction provides a flexible way to trade off between contrail reduction and fuel consumption. It can achieve a 35% contrail reduction rate with only 0.23% extra fuel consumption. The proposed fuel-efficient contrail reduction strategy provides a solution to reduce aviation-induced environmental impact on a daily basis.
  • Keywords
    aircraft control; avionics; environmental factors; fuel systems; United States airspace; aircraft cruising altitude; aviation-induced environmental impact; contrail formation reduction; contrail formation regions; cost function; fuel consumption; fuel efficient strategy; maximal reduction strategy; Aircraft; Atmospheric modeling; Fuels; Humidity; Indexes; Isobaric; Ocean temperature;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference (DASC), 2010 IEEE/AIAA 29th
  • Conference_Location
    Salt Lake City, UT
  • ISSN
    2155-7195
  • Print_ISBN
    978-1-4244-6616-0
  • Type

    conf

  • DOI
    10.1109/DASC.2010.5655533
  • Filename
    5655533