Implementation of flight control computer hardware using the C6701 processor

被引：0
|
作者：
Kwon, Jong-Kwang [1 ]
Byun, Jin-Ku [1 ]
Ahn, Jong-Min [1 ]
Ko, Joon-Soo [1 ]
Lee, Dae-Yearl [1 ]
Kim, Whan-Woo [2 ]
机构：
[1] Agcy Def Dev, Dep Aircraft, Taejon 305600, South Korea
[2] Chung Nam Natl Univ, Dep Elect Eng, Daejeon 305764, South Korea
来源：
NEW ADVANCES IN SIMULATION, MODELLING AND OPTIMIZATION (SMO '07) | 2007年
关键词：
digital flight control computer (DFLCC); SMJ320C6701; Flying Test Bed (FTB); Korean Supersonic Aircraft (KSA); flight control system (FCS); central processing unit (CPU); input output processor (IOP); rapid prototyping (RP);
D O I：
暂无
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
Flying Test Bed (FTB) program is to establish the in-house capability of digital flight control computer (DFLCC) development which will be installed on the existing Korean Supersonic Aircraft (KSA). A hardware manufacturing technology of DFLCC mainly lies in constitution and layout of central processing unit (CPU), and input output processor (IOP) board which includes core processor, with those of other boards. The FTB DFLCC has triplex digital redundancy architecture. We use to DFLCC rapid prototyping (RP) to help the participants perform design review and function analysis easily. In this paper, we present the establishment and implementation of FTB DFLCC hardware using the SMJ320C6701 processor and RP. Also, channel valid logic and cross channel data link (CCDL) are described for redundancy management.
引用
收藏
页码：352 / +
页数：2
相关论文
共 50 条
  • [31] Hardware Implementation of Smooth Region Switching for Wind Turbine Control using PDF Controller
    Li, Liuying
    Ren, Yaxing
    Jiang, Lin
    Brindley, Joseph
    Bellido-Gonzalez, Victor
    2013 INTERNATIONAL CONFERENCE ON RENEWABLE ENERGY RESEARCH AND APPLICATIONS (ICRERA), 2013, : 115 - 120
  • [32] FPGA based Improved Hardware Implementation of Booth Wallace Multiplier using Handel C
    Shinde, S. A.
    Kamat, R. K.
    ELEKTRONIKA IR ELEKTROTECHNIKA, 2011, (03) : 71 - 74
  • [33] MANIPULATOR CONTROL USING A DATA-DRIVEN MULTI-PROCESSOR COMPUTER SYSTEM.
    Egan, G.K.
    Richardson, C.P.
    Transactions of the Institution of Engineers, Australia. Mechanical engineering, 1985, ME 10 (03): : 218 - 222
  • [34] Implementation of a zero average current error control algorithm for inverters using a digital signal processor
    Baker, DM
    Agelidis, VG
    Nayar, CV
    IEEE INTERNATIONAL SYMPOSIUM ON INDUSTRIAL ELECTRONICS (ISIE 98) - PROCEEDINGS, VOLS 1 AND 2, 1998, : 450 - 455
  • [35] Assessments on Human-Computer Interaction Using Touchscreen as Control Inputs in Flight Operations
    Li, Wen-Chin
    Liang, Yung-Hsiang
    Korek, Wojciech Tomasz
    Lin, John J. H.
    ENGINEERING PSYCHOLOGY AND COGNITIVE ERGONOMICS, EPCE 2022, 2022, 13307 : 326 - 338
  • [36] Simulation and Hardware Implementation of Incremental Conductance MPPT With Direct Control Method Using Cuk Converter
    Safari, Azadeh
    Mekhilef, Saad
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2011, 58 (04) : 1154 - 1161
  • [37] Hardware Implementation of the Current Control Using the Internal Model Method in the Electric Power Steering Application
    Hu, Tsung-Hsien
    Yeh, Chih-Jung
    2009 IEEE VEHICLE POWER AND PROPULSION CONFERENCE, VOLS 1-3, 2009, : 62 - 66
  • [38] Implementation of Order reduction on TMS320C54X Processor Using Genetic Algorithm
    Desai, S. R.
    Prasad, Rajendra
    2013 ANNUAL INTERNATIONAL CONFERENCE ON EMERGING RESEARCH AREAS & 2013 INTERNATIONAL CONFERENCE ON MICROELECTRONICS, COMMUNICATIONS & RENEWABLE ENERGY (AICERA/ICMICR), 2013,
  • [39] Design and implementation of power line carrier device by using TMS320C50 processor
    Rashidi, F
    Rashidi, M
    Hashemi-Hosseini, A
    IECON'03: THE 29TH ANNUAL CONFERENCE OF THE IEEE INDUSTRIAL ELECTRONICS SOCIETY, VOLS 1 - 3, PROCEEDINGS, 2003, : 1780 - 1785
  • [40] Enabling intelligent onboard guidance, navigation, and control using reinforcement learning on near-term flight hardware
    Wilson, Callum
    Riccardi, Annalisa
    ACTA ASTRONAUTICA, 2022, 199 : 374 - 385
12345