Certifying Adaptive Flight Control Software

نویسندگان

  • Vittorio Cortellessa
  • Bojan Cukic
  • Diego Del Gobbo
  • Ali Mili
  • Marcello Napolitano
  • Mark Shereshevsky
  • Harjinder Sandhu
چکیده

As aircraft designs become more complex, automationhas become an important factor in improving safety and reliability. Automated flight control systems can respond intelligently to faults when it is impractical for a human to take control quickly. In recent years neural networks have been proposed for fault identification and accommodation purposes within flight control schemes because they are well suited to non-linear, multi-variable systems. Because neural networks learn to associate various control actions with particular input data patterns, they avoid the need to explicitly program all the relevant fault situations. A major issue in the use of adaptive fault-tolerant flight control systems is certification. Current practice relies heavily on testing as a means of performing certification. This has two shortcomings, the first being high cost. The second shortcoming of certification by testing is that it only provides a fairly limited guarantee. Certification based on testing exclusively is meaningless for new software technologies, such as adaptive controllers and neural networks which ”learn” after deployment since the system tested in the lab is not the system that is being run in the field. In this paper, we formulate the research problems underlying the certification of adaptive systems. We also describe preliminary results of a certification case study, based on the methodology which combines formal methods and automated testing, and identify the areas of basic research needed to overcome the limitations observed in the proposed framework.

برای دانلود رایگان 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

Adaptive Quaternion Attitude Control of Aerodynamic Flight Control Vehicles

Conventional quaternion based methods have been extensively employed for spacecraft attitude control where the aerodynamic forces can be neglected. In the presence of aerodynamic forces, the flight attitude control is more complicated due to aerodynamic moments and inertia uncertainties. In this paper, a robust nero-adaptive quat...

متن کامل

Adaptive Fusion of Inertial Navigation System and Tracking Radar Data

Against the range-dependent accuracy of the tracking radar measurements including range, elevation and bearing angles, a new hybrid adaptive Kalman filter is proposed to enhance the performance of the radar aided strapdown inertial navigation system (INS/Radar). This filter involves the concept of residual-based adaptive estimation and adaptive fading Kalman filter and tunes dynamically the fil...

متن کامل

Closing the Certification Gaps in Adaptive Flight Control Software

Over the last five decades, extensive research has been performed to design and develop adaptive control systems for aerospace systems and other applications where the capability to change controller behavior at different flight conditions is highly desirable. Although adaptive flight control has been partially implemented through the use of gain-scheduled control, truly adaptive control system...

متن کامل

Launch Vehicle Manual Steering with Adaptive Augmenting Control: In-Flight Evaluations of Adverse Interactions Using a Piloted Aircraft

An Adaptive Augmenting Control (AAC) algorithm for the Space Launch System (SLS) has been developed at the Marshall Space Flight Center (MSFC) as part of the launch vehicle’s baseline flight control system. A prototype version of the SLS flight control software was hosted on a piloted aircraft at the Armstrong Flight Research Center to demonstrate the adaptive controller on a full-scale realist...

متن کامل

Design of a Certifiably Dependable Next-Generation Air Transportation System

Although the authority responsible for certifying US flight control software is the Federal Aviation Administration (FAA), the US air traffic management (ATM) software to date has not been certified by the FAA or another authority in the legal sense of the word. Nevertheless, the NGATS software must be created in such a way that it is certifiably dependable because it is safety-critical softwar...

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

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2000