Adaptive Load Control for Structurally Impaired Aircraft

Autor:	Eric Y. Reichenbach, James M. Urnes, Timothy A. Smith
Rok vydání:	2010
Předmět:	Aviation safety Work (electrical) Flight envelope Computer science Control system Control (management) ComputerApplications_COMPUTERSINOTHERSYSTEMS Control engineering Envelope (motion)
Zdroj:	AIAA Infotech@Aerospace 2010.
DOI:	10.2514/6.2010-3343
Popis:	The Dynamic Flight Envelope Assessment and Prediction (DFEAP) program is a NASA funded research effort being conducted as part of NASA’s Aviation Safety Program. The goal of the DFEAP program is to provide a computational framework which will provide accurate assessment of a safe maneuvering envelope for a structurally impaired aircraft and a means to ensure the aircraft remains within this envelope. The proposed system will use the flight control system to ensure that structural limits are not exceeded. These limits are determined online by the DFEAP system. The DFEAP program will be described and work to date will be discussed.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::ca779da29597de1d365d39b4aeda9cff https://doi.org/10.2514/6.2010-3343 Zobrazit plný text záznamu