Formal Validation and Verification Framework for Model-Based and Adaptive Control Systems

被引:3
作者
Guarro, Sergio [1 ]
Ozguner, Umit [2 ]
Aldemir, Tunc [2 ]
Knudson, Matt [3 ]
Kurt, Arda [2 ]
Yau, Michael [1 ]
Hejase, Mohammad [2 ]
Kwon, Steve [2 ]
机构
[1] ASCA Inc, Redondo Beach, CA 90277 USA
[2] Ohio State Univ, Columbus, OH 43210 USA
[3] NASA, Ames Res Ctr, Moffett Field, CA 94035 USA
来源
NASA FORMAL METHODS, NFM 2016 | 2016年 / 9690卷
关键词
Validation and verification; Safety case; Model based control system; Adaptive control system; Unmanned aircraft system;
D O I
10.1007/978-3-319-40648-0_18
中图分类号
TP31 [计算机软件];
学科分类号
081202 ; 0835 ;
摘要
This paper presents the interim results of a three-year NASA project for the development of a comprehensive framework for the validation and verification (V&V) of model-based control systems and adaptive control systems (MBCSs/ACSs), with focus on Unmanned Aircraft Systems (UAS) applications. The framework applies a formal V&V methodology based on a combination of logic-dynamic model constructs and associated analysis processes, to support the generation of a documentable assurance case for a UAS control system, and to demonstrate its compliance with applicable aviation system certification standards.
引用
收藏
页码:227 / 233
页数:7
相关论文
共 8 条
[1]  
[Anonymous], P 16 IEEE INT S HIGH
[2]  
[Anonymous], 2011, RTCADO178C
[3]  
ASCA Inc., 2015, DEV FRAM VAL VER MOD
[4]   Linear and Nonlinear Controllers Applied to Fixed-Wing UAV [J].
Espinoza, Tadeo ;
Dzul, Alejandro ;
Llama, Miguel .
INTERNATIONAL JOURNAL OF ADVANCED ROBOTIC SYSTEMS, 2013, 10
[5]  
Fossen T. I., 2011, MATH MODELS CONTROL
[6]  
Guarro S., 2012, P 11 INT C PROB SAF
[7]  
Ozguner U., 1990, P 5 IEEE INT S INT C, V1, P2
[8]  
U. S. Nuclear Regulatory Commission, 2009, NUREGCR6985