Feasibility Demonstration of an Aircraft Performance Risk Assessment Model

نویسندگان

  • Alex Smith
  • Rick Cassell
  • Y. Eric Yang
چکیده

This paper presents the development of an Aircraft Performance Risk Assessment Model (APRAM). The model consists of a set of software tools that processes aircraft data available from Digital Flight Data Recorders (DFDRs) and Quick Access Recorders (QARs) to identify precursor events and compute incident and accident risks. The feasibility version of the generic risk assessment model is limited in scope to controlled flight towards terrain (CFTT) and controlled flight into terrain (CFIT) incident and accident types respectively. The objective of this research is to develop a computer model that uses both empirical data and expert judgement to quantify the risk of an incident and/or accident. The general approach taken in assessing risk is to develop an automated means of analyzing commercial aircraft flight recorder data from routine flights, combining the use of exceedance information from the data with information about the contextual factors that are not directly available from the data recorders. Expert opinion is incorporated through the use of knowledge-based rules. This information is analyzed to identify incident and/or accident precursors and their contributing factors. The output from the model is a risk estimate that includes consequence, severity, and probability of occurrence, similar to that used for aircraft certification.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

In-Trim Flight Investigations of a Conceptual Fluidic Thrust-Vectored Unmanned Tail-Sitter Aircraft

The feasibility of using a stand alone Fluidic Thrust-Vectoring (FTV) system for the purpose of longitudinal trim of an unmanned aerial vehicle is the focus of the research presented in this paper. Since the fluidic thrust vectoring requires high pressure secondary air to deflect the engine exhaust gases, this research also provides an analytical toolset for preliminary sizing of a suitable sec...

متن کامل

On the Integration of Human Performance and Collision Risk Simulation Models of Runway Operation

The integration of a human performance model (Air Man-machine Integration Design and Analysis System, Air MIDAS) and an accident risk assessment methodology (Traffic Organization and Perturbation AnalyZer, TOPAZ) was investigated in order to learn about the similarities and differences of their models, to demonstrate the feasibility of such integration, and the integration impact on accident ri...

متن کامل

Introduse and Need Assessment of Regional Aircrafts by Software and Modeling

An analysis was conducted to examine the market visibility of small aircraft as a transportation mode in competition with automobile and scheduled commercial air travel by estimating the pool of users that would potentially switch on-demand air travel due to cost/time saving. These new aircraft greatly increase the practicality of regional aircraft as a transportation mode that can avoid the co...

متن کامل

Numerical and Neural Network Modeling and control of an Aircraft Propeller

In this paper, parametric and numerical model of the DC motor, connected to aircraft propellers are extracted. This model is required for controlling trust and velocity of the propellers, and consequently, an aircraft. As a result, both of torque and speed of the propeller can be controlled simultaneously which increases the kinematic and kinetic performance of the aircraft. Parametric model of...

متن کامل

Fuzzy Model of Human’s Performance for Guarding a Territory in an Air Combat

This paper proposes a new method for a three dimensional fuzzy model of pilot's performance for guarding a territory with a short-distance between two aircraft in an air combat task with a gun. A third-order nonlinear point mass vehicle model is considered for an aircraft's flight dynamics. The desired value of the velocity, the flight path and the heading angles are obtained from some derived ...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2000