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检索条件"机构=Aviation Key Laboratory of Science and Technology on Airborne and Missile-borne Computer"

共 51 条记录，以下是11-20 订阅

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Fault-Tolerant Filtering Algorithm for SINS/BDS Tightly-coupled Integrated Navigation System

Fault-Tolerant Filtering Algorithm for SINS/BDS Tightly-coup...

引用

2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

作者： Benchuan, Zhou Hao, Lu Jianyun, Xu Hongob, Zhang China Airborne Missile Academy Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons Henan471099 China PLA's Military Representative Office in China Airborne Missile Academy Henan471099 China

ISBN: (纸本)9781538611715

The effective fault diagnosis is the basis of system reliability and accuracy in SINS/BDS tightly-coupled integrated navigation system. The state equation and measurement equation in the launch inertial frame are modeled. A fault-tolerant Kalman filtering algorithm is proposed, the improved chi-square test method is designed to realize the detection and screening of BDS measurement fault. The simulation results illustrate that the fault-tolerant Kalman filter can effectively detect faults, the velocity error and the position error are controlled within 0.3m/s and 20m repectively. © 2018 IEEE.

关键词： Kalman filters

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An Architecture Modeling and Simulation Methods of Integrated Electromechanical Management System

An Architecture Modeling and Simulation Methods of Integrate...

引用

International Conference on Computational Intelligence and Security

作者： Peng Guo Yunming Sun Wei Niu Chong Qin Aviation Key Laboratory of Science and Technology on Airborne and Missile-borne Xi'an China

ISBN: (纸本)9781509048410

airborne integrated electromechanical management system (IEMS) is a safety critical system, ensuring the aircraft normal flight and the normal operation of each function of the plane. This paper analyses IEMS of the current fighter aircraft, EAP, F-22 and F-35, proposes an architecture modeling and simulation method of IEMS. This method establishes a common model of IEMS, forms modeling and simulation process of IEMS, detailed designs monitoring and redundancy management algorithms based Simulink. Finally, we have applied the methodology on a commercial aircraft and verify the feasibility, accuracy and effectiveness of the modeling method.

关键词： Atmospheric modeling Monitoring Aircraft Redundancy computer architecture Aerospace control Aerospace electronics

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A UML Model to Simulink Model Transformation Method in the Design of Embedded Software

A UML Model to Simulink Model Transformation Method in the D...

引用

International Conference on Computational Intelligence and Security

作者： Peng Guo Yahui Li Peng Li Shuai Liu Dongya Sun Aviation Key Laboratory of Science and Technology on Airborne and Missile-borne Xi'an China

ISBN: (纸本)9781479974351

Model Driven Development is becoming the trend of embedded software development, UML and Simulink are very important modeling languages. However, UML is a semi-formal modeling language, lacking of accurate semantics, which can't validate correctness of embedded software development. To solve this problem, this paper presents a model transformation method between UML design model and Simulink simulation model. The method consists of UML StateMachine meta-model, Simulink/Stateflow meta-model and a set of mapping rules from UML meta-model to Simulink meta-model. Last we apply this method to flight control software of autopilot system. The method implements automatic transformation from UML to Simulink, improving development efficiency of embedded software, and providing technique support for embedded software development, such as automobile control system, express control system, and avionics system.

关键词： Unified modeling language Software packages Mathematical model Computational modeling Atmospheric modeling Embedded software

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Nonlinear Robust Attitude Tracking Control of 3-DOF Helicopter Based on Output Feedback

Nonlinear Robust Attitude Tracking Control of 3-DOF Helicop...

引用

International Conference on Guidance, Navigation and Control, ICGNC 2022

作者： Yu, Jingwei Peng, Chen Zhang, Longteng He, Xiaohua University of Electronic Science and Technology of China Chengdu611731 China China Airborne Missile Academy Luoyang471099 China Aviation Key Laboratory of Science and Technology on Airborne Guided Weapon Luoyang471099 China

ISBN: (纸本)9789811966125

Three-channel attitude tracking problem is studied for an underactuated three degree of freedom (3-DOF) helicopter with only angular position measurements in this paper. To deal with the underactuated characteristics of the helicopter, an inner-outer loop structure is adopted to achieve attitude tracking of three coupling channels, i.e., the elevation, travel and pitch channels, only using two control inputs. Then, a nonlinear robust controller is proposed for each channel of the helicopter to implement accurate attitude tracking via output feedback. An auxiliary system with second order and filtered error signals are also considered in the controller. Moreover, to mitigate the effects of uncertainties and disturbances involved in the system, an uncertainties and disturbances estimator (UDE) is incorporated into controller. Simulation results are shown to illustrate feasibility of presented controller. © 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.

关键词： Helicopters

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A Real-Time Sensor Guided Runway Detection Method for Forward-Looking Aerial Images

A Real-Time Sensor Guided Runway Detection Method for Forwar...

引用

International Conference on Computational Intelligence and Security

作者： Jingzhe Wang Yue Cheng Jianchun Xie Wensheng Niu Aeronautics Computing Technique Research Institute Aviation Key Laboratory of Science and Technology on Airborne and Missile-borne Computer Xi'an China

ISBN: (纸本)9781467386616

With the development of avionics technology, the runway detection technique becomes increasingly important both in military and civil applications. But the existing runway detection methods are mostly intended for satellite images or downward-looking aerial photos and the algorithm complexity is relatively high, which makes it hard to apply them to airborne real-time applications. In this paper, a real-time sensor guided runway detection method is presented. First of all, with the help of sensor data and terrain data from EVS and SVS, a runway template is generated and a search region is therefore determined. Then within the search region, a lines extraction on query image is performed. And finally the matching process is applied to the query image and template to detect the runway area. Experimental results on simulation system and real aerial images show that the proposed approach has a high precision and an 87.7% less time cost than an existing state-of-art matching method.

关键词： Real-time systems Image edge detection Cameras Airports Feature extraction Complexity theory Machine vision

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Terminal Angle Constraint Guidance Law Based on SDRE Method 4

Terminal Angle Constraint Guidance Law Based on SDRE Method

引用

2018 4th International Conference on Energy Equipment science and Engineering, ICEESE 2018

作者： Zhou, Shaobo Luo, Delin Zhang, Jinpeng School of Aerospace Engineering Xiamen University Xiamen Fujian361102 China Aviation Key Laboratory of Science Technology on Airborne Guided Weapon China Airborne Missile Academy Luoyang Henan471009 China

In this paper, a new guidance law based on SDRE method is designed to solve the problem of terminal angle constraint of a missile by using nonlinear kinematics model and dynamic model of a missile. The constraint of collision angle can be realized by the guidance law under the condition of satisfying the requirement of miss distance of terminal guidance. In addition, the guidance instructions in the form of feedback and the analytic solution of the guidance law are obtained in the two-dimensional plane. Compared with previous terminal guidance methods, the advantage of the method is that it does not depend on the estimation of the time to go. The effectiveness of the proposed guidance law can be verified by digital simulation. © 2019 Published under licence by IOP Publishing Ltd.

关键词： missiles

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Design and Realization of Intelligent airborne Information Processing Concept Simulation System 24

Design and Realization of Intelligent Airborne Information P...

引用

24th IEEE International Conference on High Performance Computing and Communications, 8th IEEE International Conference on Data science and Systems, 20th IEEE International Conference on Smart City and 8th IEEE International Conference on Dependability in Sensor, Cloud and Big Data Systems and Application, HPCC/DSS/SmartCity/DependSys 2022

作者： Xie, Jianchun Bai, Linting Luo, Qing Aviation Key Laboratory of Science and Technology on Airborne and Missile-borne Computer Avic Xi'an Aeronautics Computing Technique Research Institute Xi'an China College of Aerospace Engineering Nanjing University of Aeronautics and Astronautics Nanning China Shenyang Aircraft Design and Reserch Institute Shenyang China

ISBN: (纸本)9798350319934

Facing the development trend of future distributed cloud operations, intelligent operations, and the technical requirements of multi-machine collaborative operations in the aviation field, this paper further studies the unified data transmission and management of multiple platforms based on the research of the unified cloud intelligent combat system architecture. Distributed data storage and management, multi-platform open information processing resource management and other key technologies, on the basis of the principle prototype designed and implemented by ourselves, a set of conceptual simulation platforms have been constructed for the simulation and technical verification of the entire airborne information processing system. © 2022 IEEE.

关键词： Distributed cloud

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The airborne Information Processing System Development Research 7

The Airborne Information Processing System Development Resea...

引用

7th International Conference on Dependable Systems and Their Applications, DSA 2020

作者： Xie, Jianchun Li, Yahui Wang, Zhonghua Bai, Linting Xi'an Aeronautics Computing Technique Research Institute Avic Aviation Key Laboratory of Science and Technology on Airborne and Missileborne Computer Xi'an China

ISBN: (数字)9780738124223

ISBN: (纸本)9780738124223

the airborne information processing system, which is subordinate to the avionics system, is the basic sub-system performing information data processing in the aircraft platform. It provides computing, storage, information transmission and other basic resources for the whole aircraft, and can provide various functions and services such as computing, management, configuration, scheduling and other. The future development of airborne information processing system should be driven by the basic computer technology development and military requirements of aircraft platform. From these two perspectives, on the basis of full analysis of the development status, this paper summarizes the future airborne information processing system architecture and some key technical characteristics of the processing platform, laying a foundation for future research work. © 2020 IEEE.

关键词： Scheduling

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Implementation of Multi-level Security Domain Scheme for Embedded computer Based on MILS Architecture 5

Implementation of Multi-level Security Domain Scheme for Emb...

引用

5th IEEE International Conference on computer and Communications, ICCC 2019

作者： Zhong-Hua, Wang Sha-Sha, G.A.O. Ya-Hui, L.I. Xi'An Aeronautics Computing Technique Research Institute AVIC Aviation Key Laboratory of Science and Technology Airborne and Missileborne Computer Xi'an China

ISBN: (纸本)9781728147437

For multiple embedded computers working together, the functional failure resulting from the underlying hardware or system crash will cause a sudden abort of applications. Different types of applications may have security requirements for data isolation and access control. Therefore, we propose a scheme to implement multi-level security domain dynamic management oriented embedded computers based on MILS architecture. Firstly, the scheme builds local security policy items and access control lists according to type, function and security level. After that, security domain of all applications is constructed to achieve the safety purpose that applications can perform migration cross partitions and cross platforms. Our experiments and analysis show that the proposed scheme is feasible and correct. © 2019 IEEE.

关键词： Access control

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Heterogeneous computing platform based on CPU+FPGA and working modes 12

Heterogeneous computing platform based on CPU+FPGA and worki...

引用

12th International Conference on Computational Intelligence and Security, CIS 2016

作者： Li, Yang Zhao, Xiaodong Cheng, Taoran Xi'an Aeronautics Computing Technique Research Institute AVIC Aviation Key Laboratory of Science and Technology on Airborne and Missileborne Computer Xi'an710065 China

ISBN: (纸本)9781509048403

Currently, with the development of high performance computing, multicore system and heterogeneous system have become the transformation that is taking place. However, Promoting performance of processor has encountered bottlenecks of heat and power by means of Moore's Law;one or more CPUs can't meet requiremen s of a large number of computing. The use of Heterogeneous Computing Platform is becoming an inexorable trend of high performance computing. This paper introduced the Heterogeneous Computing Platform and CPU+FPGA Heterogeneous Computing Platform, analysis the architecture, characteristics and working modes of CPU+FPGA Heterogeneous Computing Platform. © 2016 IEEE.

关键词： Field programmable gate arrays (FPGA)

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