Verification Challenges in F-16 Ground Collision Avoidance and Other Automated Maneuvers

ARCH@ADHS Pub Date : 2018-09-17 DOI:10.29007/91x9
Peter Heidlauf, Alexander Collins, M. Bolender, Stanley Bak
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引用次数: 35

Abstract

Benchmark Proposal: The F-16 Fighting Falcon is a highly-maneuverable aircraft in production since the 1970s. Since then, several studies and books have investigated the aircraft’s performance and created simulation models. In this paper, we present some of these models as a verification challenge, providing MATLAB and Python code to simulate an F-16 performing ground collision avoidance as well as other autonomous maneuvers. The aircraft model and inner-loop controller has 16 continuous variables with piecewise nonlinear differential equations. Autonomous maneuvers are performed by an outer-loop controller using finite-state machines with guards involving the continuous variables. Passfail specifications are provided based on the aircraft flight limits and boundaries of the model. This model aims to be a starting point for analyzing detailed behaviors of aerospace systems.
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F-16地面避碰和其他自动机动的验证挑战
基准建议:F-16战斗猎鹰是一种高机动性飞机,自20世纪70年代开始生产。从那时起,几项研究和书籍调查了飞机的性能并创建了仿真模型。在本文中,我们提出了其中一些模型作为验证挑战,提供MATLAB和Python代码来模拟F-16执行地面避碰以及其他自主机动。飞行器模型和内环控制器具有16个连续变量,具有分段非线性微分方程。自主机动由外环控制器使用有限状态机执行,该有限状态机具有涉及连续变量的保护。通行证规格是根据飞机的飞行限制和模型的边界提供的。该模型旨在成为分析航空航天系统详细行为的起点。
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ARCH-COMP18 Category Report: Hybrid Systems Theorem Proving Linear Differential-Algebraic Equations (Benchmark Proposal) Verification Challenges in F-16 Ground Collision Avoidance and Other Automated Maneuvers Discrete-Space Analysis of Partial Differential Equations ARCH-COMP18 Category Report: Hybrid Systems with Piecewise Constant Dynamics
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