English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Tools annual

Global: Zendy Free Plan

Global: Zendy Tools monthly

Global: Zendy Plus monthly

The paper deals with an architecture of fuel tanks onboard an aircraft. The fuel consumption mode has a great influence above the position of aircraft’s center of gravity; the authors have determined the position of each fuel tank center of gravity and have also determined its space trajectory during the fuel consumption. When a malfunction of the fuel consumption occurs, aircraft’s center of gravity might be displaced outside the safety envelope, which might badly influence the stability of the aircraft and, because of the autopilot intervention, it might also increase aircraft attitude, its total drag, as well as the specific fuel consumption of aircraft engines. The authors have designed a subroutine for restore the stability, by reordering the fuel consumption to rebalance the aircraft, to restore aircraft attitude and to reduce the engine’s specific fuel consumption initially increased by the drag.

METHOD OF CONTROL OF AIRCRAFT CENTER OF GRAVITY BASED ON THE FUEL CONSUMPTION ORDER