Results 81 to 90 of about 692 (185)

Design of a wing tip device for active maneuver and gust load alleviation [PDF]

open access: yes, 2018
In the present work the design of a wing tip device is presented along with the definition of the maneuver load controller and the gust load controller.
Fonte, Federico   +5 more
core   +1 more source

Gust Load Alleviation on a Large Blended Wing Body Airliner

open access: yes, 2010
This paper investigates the gust load response of a large 750 passenger Blended Wing Body (BWB) airliner for identification of sizing cases for the aircraft structure.
Aversa, N.   +8 more
core  

Multidisciplinary Simulation for Gust Load Alleviation Control Surface Analysis [PDF]

open access: yes, 2018
The structural dimensioning of an airplane will be significantly influenced by gust, maneuver and ground loads. Adaptive load alleviations methods (keyword: 1g-wing) promise the potential reducing the maximum loads and therefore the structural weight ...
Lars Reimer   +3 more
core   +1 more source

Recasting Discrete 1-Cosine Gust Requirements as Frequency Domain Specifications for Load Alleviation Control Design

open access: yes, 2022
In the context of active gust- and turbulence-load alleviation function design, control designers optimize the response of the closed-loop system to satisfy the criteria of the certification specifications (e.g. EASA CS-25.341). This includes time-domain
Cavaliere, Davide, Fezans, Nicolas
core   +1 more source

Coherent Lidar Turbulence Measurement for Gust Load Alleviation

open access: yes, 1996
Atmospheric turbulence adversely affects operation of commercial and military aircraft and is a design constraint. The airplane structure must be designed to survive the loads imposed by turbulence.
David Soreide   +3 more
core   +1 more source

Active Gust Load Alleviation for Flexible Wing Aircraft

open access: yes, 2017
This paper presents a novel active gust load alleviation approach within a multi-objective flight control framework developed by NASA for a flexible wing aircraft. The aircraft model is based on the NASA Generic Transport Model (GTM). The wing structures
Ferrier, Y.L. (author)
core  

An Unusual Structure for a Feedforward Gust Load Alleviation Controller [PDF]

open access: yes, 2017
This paper presents an unusual feedforward controller structure that allows to take allocation constraints into account which can be expressed in the time-frequency or time-scale domains. This novel controller structure was motivated by the design of a feedforward controller for airplane gust and turbulence load alleviation based on Doppler LIDAR ...
openaire   +1 more source

Gust Load Alleviation Based on Model Predictive Control [PDF]

open access: yes
Weight reduction is a typical design goal for modern aircraft. If gust encoun- ters (as required by Certification Specification 25) are sizing conditions of parts of the airframe, this can be achieved (for example) by an active gust load alleviation ...
Giesseler, Hans-Gerd   +4 more
core  

Decentralized Control of Ailerons for Gust Load Alleviation [PDF]

open access: yes
This paper describes the design of a so-called decentralized gust load alleviation system for an aircraft with high aspect ratio wings. The system uses control loops at each individual aileron actuator that aim to reduce local structural dynamics at each respective point of installation in the wing structure. To this end, each actuator is equipped with
Michel, Kolja   +3 more
openaire   +1 more source

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