Feasibility study on fixed flight-path angle descent for wide-body passenger aircraft


== Abstract ==

This study proposes the use of fixed flight-path angle (FPA) descent as a potential alternative for eco-friendly air traffic operations. Additionally, given that the proposed descent procedure follows a fixed, assigned flight-path angle, with the aircraft continuously descending toward the runway threshold with near-idle thrust, the trajectory should be more predictable for air-traffic controllers. As such, the proposed approach is expected to contribute significantly toward decreasing the air traffic fuel consumption, while simultaneously facilitating the air traffic controllers’ task of maintaining the required time spacing between concurrent traffic. Furthermore, FPA descent does not require any retrofits in the fundamental components of current ground systems and/or onboard avionics. This paper clarifies the feasibility of fixed flight-path angle descent for B777-200 and B787-8 wide-body jet passenger aircraft, envisaging its implementation in near-term operations. A total of 30 trials were carried out in a series of experiments designed to evaluate the proposed descent method, considering arrivals at two major international airports in Japan—the Tokyo and Kansai International Airports—using B777-200 and B787-800 full flight simulators of a national airline. The pilots’ procedures, cockpit operability, assigned vertical path tracking performance, and fuel efficiency associated with the proposed FPA descent are discussed and compared with those of conventional arrival operations. The analysis results indicate that the fixed flight-path angle descent is feasible for large-sized jet aircraft within the assumed operational environment, and that its combined use with speed control has the potential to result in even better energy-saving performance in future air traffic management operations.

Document type: Article

== Full document ==
<pdf>Media:Draft_Content_359910654-beopen968-6726-document.pdf</pdf>


== Original document ==

The different versions of the original document can be found in:

* [http://dx.doi.org/10.1007/s13272-018-0337-9 http://dx.doi.org/10.1007/s13272-018-0337-9] under the license https://creativecommons.org/licenses/by

* [https://link.springer.com/content/pdf/10.1007/s13272-018-0337-9.pdf https://link.springer.com/content/pdf/10.1007/s13272-018-0337-9.pdf] under the license https://creativecommons.org/licenses/by/4.0

* [http://link.springer.com/content/pdf/10.1007/s13272-018-0337-9.pdf http://link.springer.com/content/pdf/10.1007/s13272-018-0337-9.pdf],
: [http://link.springer.com/article/10.1007/s13272-018-0337-9/fulltext.html http://link.springer.com/article/10.1007/s13272-018-0337-9/fulltext.html],
: [http://dx.doi.org/10.1007/s13272-018-0337-9 http://dx.doi.org/10.1007/s13272-018-0337-9] under the license cc-by

* [https://link.springer.com/article/10.1007/s13272-018-0337-9 https://link.springer.com/article/10.1007/s13272-018-0337-9],
: [https://trid.trb.org/view/1605051 https://trid.trb.org/view/1605051],
: [https://paperity.org/p/162820891/feasibility-study-on-fixed-flight-path-angle-descent-for-wide-body-passenger-aircraft https://paperity.org/p/162820891/feasibility-study-on-fixed-flight-path-angle-descent-for-wide-body-passenger-aircraft],
: [https://academic.microsoft.com/#/detail/2898173216 https://academic.microsoft.com/#/detail/2898173216] under the license https://creativecommons.org/licenses/by/4.0