Aviate, Navigate: Functional Visualizations of Asymmetric Flight Envelope Limits

2021 ◽  
pp. 1-16
Author(s):  
Tom A. D. T. Rijndorp ◽  
Clark Borst ◽  
Coen C. de Visser ◽  
Olaf Stroosma ◽  
Marinus M. van Paassen ◽  
...  
Keyword(s):  
Author(s):  
Dirk Van Baelen ◽  
M. M. (René) van Paassen ◽  
Joost Ellerbroek ◽  
David A. Abbink ◽  
Max Mulder

2019 ◽  
Author(s):  
Anhad Singh Bajaj

The ATR 72 is a twin-engine turboprop, short-haul regional airliner developed and produced in France and Italy by aircraft manufacturer ATR (Aerei da Trasporto Regionale or Avions de transport régional), a joint venture formed by French aerospace company Aérospatiale (now Airbus) and Italian aviation conglomerate Aeritalia (now Leonardo S.p.A.). The number "72" in its name is derived from the aircraft's standard seating configuration in a passenger-carrying configuration, which could seat 72–78 passengers in a single-class arrangement.


1994 ◽  
Author(s):  
Zuu-Chang Hong ◽  
Shyuan-Jye Chen ◽  
Jeng-Shing Chern
Keyword(s):  

2018 ◽  
Vol 67 ◽  
pp. 368-380 ◽  
Author(s):  
Thomas Lombaerts ◽  
Gertjan Looye ◽  
Andreas Seefried ◽  
Miguel Neves ◽  
Tobias Bellmann

2007 ◽  
Vol 129 (4) ◽  
pp. 962-969 ◽  
Author(s):  
Randal T. Rausch ◽  
Kai F. Goebel ◽  
Neil H. Eklund ◽  
Brent J. Brunell

In-flight fault accommodation of safety-critical faults requires rapid detection and remediation. Indeed, for a class of safety-critical faults, detection within a millisecond range is imperative to allow accommodation in time to avert undesired engine behavior. We address these issues with an integrated detection and accommodation scheme. This scheme comprises model-based detection, a bank of binary classifiers, and an accommodation module. The latter biases control signals with pre-defined adjustments to regain operability while staying within established safety limits. The adjustments were developed using evolutionary algorithms to identify optimal biases off-line for multiple faults and points within the flight envelope. These biases are interpolated online for the current flight conditions. High-fidelity simulation results are presented showing accommodation applied to a high-pressure compressor fault on a commercial, high-bypass, twin-spool, turbofan engine throughout the flight envelope.


2006 ◽  
Vol 39 (9) ◽  
pp. 53-58 ◽  
Author(s):  
Prathyush P. Menon ◽  
Declan G. Bates ◽  
Ian Postlethwaite

2015 ◽  
Author(s):  
Brent S. Paul

The successful integration of aviation capabilities aboard ships is a complex endeavor that must balance ship design with the flight envelope of the helicopter. This can be particularly important when considering air wakes and other flow around the superstructure as it impacts the flight deck. This flow can generate unsteady structures that may interfere with safe helicopter operations. Computational fluid dynamics (CFD) is commonly used to characterize the flow field and assess potential impacts to the flight envelope, which can be used to help define an operating envelope for helicopter operations.


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