scispace - formally typeset
Journal ArticleDOI

Enhanced self-spacing algorithm for three-degree decelerating approaches

TLDR
A flap scheduling algorithm with complementary interface has been developed that takes noise nuisance and in-trail spacing into account and confirmed the conflict-free performance benefits and the feasibility of self-spacing during continuous decelerating/descent approaches under actual flight conditions.
Abstract
A current trend in aircraft noise abatement around airports is exploiting the benefits of revised arrival and approach procedures with computational aids, such as onboard and ground-based trajectory prediction algorithms and displays. The challenge for these upcoming advanced noise abatement procedures is to mitigate the noise impact without sacrificing runway capacity. A proposed solution, implemented in the three-degree decelerating approach, is to delegate the task of spacing the aircraft to the cockpit during the approach. To assist the pilots, a flap scheduling algorithm with complementary interface has been developed that takes noise nuisance and in-trail spacing into account The design and functionality of this support system is presented and evaluated with three experiments. Monte Carlo simulations indicated adequate and consistent performance and robustness of the self-spacing algorithm for various wind and traffic scenarios. A pilot-in-the-loop simulator experiment verified that, with the aid of the algorithm, pilots were able to execute the noise abatement procedure consistently while maintaining safe spacing. The support system reduced pilot workload up to an effort level comparable to current standard approaches. The concept was demonstrated in flight, which confirmed the conflict-free performance benefits and the feasibility of self-spacing during continuous decelerating/descent approaches under actual flight conditions.

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Citations
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Journal ArticleDOI

Fault Tolerant Sliding Mode Control Design with Piloted Simulator Evaluation

TL;DR: In this paper, the authors considered sliding mode allocation schemes for fault tolerant control, which allow redistribution of the control signals to the remaining functioning actuators when a fault or failure occurs. But the results obtained from implementing the controllers on a research flight simulator, configured to represent a B747 aircraft, show good performance in both nominal and failure scenarios, even in wind and gust conditions.
Journal ArticleDOI

Time and Energy Management During Descent and Approach: Batch Simulation Study

TL;DR: In this paper, a novel integrated planning and guidance concept is developed that optimizes aircraft trajectories from top of descent to the runway threshold to achieve a continuous engine-idle descent.
Journal ArticleDOI

Wind-Profile Estimation Using Airborne Sensors

TL;DR: A method for real-time estimation of a wind profile in the terminal maneuvering area, based on data transmitted by nearby aircraft, usable for accurate trajectory prediction to improve continuous-descent operations and spacing performance.
Proceedings ArticleDOI

Continuous Descent Approaches with Variable Flight-Path Angles under Time Constraints

TL;DR: Investigating the influence of multiple segments with different flight-path angles on the time of arrival finds a new procedure with Variable Flight-path angle (VFA) involving active planning of the approach from the pilot through a pilot support interface, presented in the Vertical Situation Display.
Journal ArticleDOI

Investigating string stability of a time-history control law for Interval Management

TL;DR: In this paper, a simplified, closed-form string stability analysis for a time-history speed control law, which has been proposed for interval management, is presented, and simulation results are used to evaluate string behavior and system performance for an approach-spacing operation.
References
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Book ChapterDOI

Development of NASA-TLX (Task Load Index): Results of Empirical and Theoretical Research

TL;DR: In this article, the results of a multi-year research program to identify the factors associated with variations in subjective workload within and between different types of tasks are reviewed, including task-, behavior-, and subject-related correlates of subjective workload experiences.
Journal ArticleDOI

Models of Man.

G. L. S. Shackle, +1 more
- 01 Nov 1957 - 
Journal ArticleDOI

Continuous Descent Approach: Design and Flight Test for Louisville International Airport

TL;DR: In this paper, a design methodology based on the principles of system analysis was used to design a noise abatement approach procedure for Louisville International Airport, which was shown to reduce the A-weighted peak noise level at seven locations along the flight path by 3.9 to 6.5 dBA and reduce the fuel consumed during approach by 400 to 500 lb.
Proceedings ArticleDOI

Achieving low approach noise without sacrificing capacity

TL;DR: A modified three degree decelerating approach (MTDDA) is introduced that provides the same noise benefits as the TDDA with little or no loss in capacity relative to conventional approach procedures.
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