A Flight Control System for a Vehicle

被引:0
|
作者
Tanjim, Meer Shadman Shafkat [1 ]
Oishi, Ashrafun Nushra [1 ]
Nandy, Animesh [1 ]
Jannah, Raihanul [1 ]
Ahmed, Sakib [1 ]
机构
[1] Amer Int Univ Bangladesh, Dept Elect & Elect Engn, Dhaka, Bangladesh
关键词
Universal Flight System (USF); Instant flight facility (IFF); Bernoulli's principle; Duct theory; Emergency transportation; Flight Control System (FCS); Futuristic Vehicle Upgrade; Traffic Jam solution; Transport problem; Revolution;
D O I
10.1109/icrest.2019.8644151
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The most common problem of a city is its traffic jam in busy and important areas. Nevertheless, ideas have already been pragmatic, traffic jam can't be controlled completely nor it gets alternative. Vehicles are increasing in the proportion of population growth and technological enrichment. Moreover, road blockage, emergency aspects, armed security purpose etc. are also a fact to be solved now-a days. Therefore, we have got an idea of overpassing the vehicles so that the road becomes traffic free. After researching various theories with the help of Bernoulli's principle and duct theory, a new standard flight control system has been visualized. Here, a balanced, portable, comfortable and a universal system with instant flight facility has been introduced, which is more advantageous than quadcopter system. The system can be installed on any existing vehicle with an initial feature of instant flight and forward-backward movement along with left/right turns later. After having a lift, the vehicle can move on the air like a comfortable jerk-less vehicle on the road.
引用
收藏
页码:313 / 318
页数:6
相关论文
共 50 条
  • [1] Flight Control System of Unmanned Aerial Vehicle
    浦黄忠
    甄子洋
    夏曼
    Transactions of Nanjing University of Aeronautics and Astronautics, 2015, 32 (01) : 1 - 8
  • [2] Design of Control System for a Quadrotor Flight Vehicle
    Bayir, R.
    Cosgun, A. E.
    INTELLIGENT TECHNOLOGIES IN LOGISTICS AND MECHATRONICS SYSTEMS, ITELMS 2013, 2013, : 55 - 59
  • [3] Decoupling the flight control system of a supersonic vehicle
    Tsay, Tain-Sou
    AEROSPACE SCIENCE AND TECHNOLOGY, 2007, 11 (7-8) : 553 - 562
  • [4] Flight control system design for a micro aerial vehicle
    Guglieri, G
    Pralio, B
    Quagliotti, F
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2006, 78 (02): : 87 - 97
  • [5] A Flight Control System for Small Unmanned Aerial Vehicle
    Tunik A.A.
    Nadsadnaya O.I.
    International Applied Mechanics, 2018, 54 (02) : 239 - 247
  • [6] Flight Control System of a Robotic Portable Unmanned Aerial Vehicle
    Rao, Jinjun
    Gao, Tongyue
    Jiang, Zhen
    Gong, Zhenbang
    2ND IEEE INTERNATIONAL CONFERENCE ON ADVANCED COMPUTER CONTROL (ICACC 2010), VOL. 1, 2010, : 540 - 544
  • [7] Control of an air-ground amphibious vehicle flight system
    Wang, Zheng-Jie
    Ma, Jian
    Zhu, Hang
    Wang, Jian-Zhong
    Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, 2015, 35 (12): : 1257 - 1261
  • [8] Design of invariant control system for longitudinal motion of flight vehicle
    S. A. Krasnova
    N. S. Mysik
    Automation and Remote Control, 2011, 72 : 2100 - 2111
  • [9] Design of Invariant Control System for Longitudinal Motion of Flight Vehicle
    Krasnova, S. A.
    Mysik, N. S.
    AUTOMATION AND REMOTE CONTROL, 2011, 72 (10) : 2100 - 2111
  • [10] Robustness assessment for flight control system of an oceanographic unmanned aerial vehicle
    李蒙
    刘莉
    VERES S. M.
    Journal of Beijing Institute of Technology, 2011, 20 (02) : 158 - 167