Simplified Model Building of Mini Unmanned Helicopter in Hover

被引：1
|
作者：
Wu, Jiande [1 ]
Fan, Yugang [1 ]
Feng, Ting [1 ]
Chao, Yi [2 ]
机构：
[1] Kunming Univ Sci & Technol, Fac Informat Engn & Automat, Kunming, Peoples R China
[2] Yunnan Univ, Natl Pilot Sch Software, Kunming, Peoples R China
来源：
2ND IEEE INTERNATIONAL CONFERENCE ON ADVANCED COMPUTER CONTROL (ICACC 2010), VOL. 5 | 2010年
关键词：
simplified model; mini unmanned helicopter; hover; nonlinear;
D O I：
10.1109/ICACC.2010.5486797
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The reduced model of mini unmanned helicopter in hover is proposed in this paper. A specific analysis for the dynamic characteristics of mini unmanned helicopter is given. Based on the analysed results, we carry on a very thorough trim computing process under the condition that the mini unmanned helicopter stays in hover. We can use the 6-DOF rigid body equations of motion to establish a full state nonlinear equation for mini unmanned helicopter. Further, by taking a small disturbance linearization method, we can deduce a small disturbance linear differential equation of motion for the mini unmanned helicopter of constant motion. We believe this model means a lot to autonomous hover control.
引用
收藏
页码：626 / 629
页数：4
相关论文
共 50 条
  • [21] SURFACE PRESSURE MEASUREMENTS AT TIP OF A MODEL HELICOPTER ROTOR IN HOVER
    SHIVANANDA, TP
    MCMAHON, HM
    GRAY, RB
    JOURNAL OF AIRCRAFT, 1978, 15 (08): : 460 - 467
  • [22] A coupled CFD and wake model simulation of helicopter rotor in hover
    Zhao, Qinghe
    Li, Xiaodong
    3RD INTERNATIONAL CONFERENCE ON ENERGY EQUIPMENT SCIENCE AND ENGINEERING (ICEESE 2017), 2018, 128
  • [23] Helicopter industry stuck in a hover
    Phillips, EH
    AVIATION WEEK & SPACE TECHNOLOGY, 1999, 150 (08): : 42 - +
  • [24] LQR based PID controller design for model helicopter in hover
    Kim, Moo Seok
    Kim, Joon Ki
    Han, Jeong Yup
    Park, Hong Bae
    3RD INTERNATIONAL CONFERENCE ON COMPUTING, COMMUNICATIONS AND CONTROL TECHNOLOGIES, VOL 1, PROCEEDINGS, 2005, : 155 - 160
  • [25] HOVER PERFORMANCE ANALYSIS OF COAXIAL MINI UNMANNED AERIAL VEHICLE FOR APPLICATIONS IN MOUNTAIN TERRAIN
    Ramesh, P. S.
    Lal, Jeyan J. V. Muruga
    AVIATION, 2022, 26 (02) : 112 - 123
  • [26] The Flight Control Design of Mini Unmanned Helicopter on Sliding Mode Control
    Guo, Xijin
    Sun, Wei
    Li, Zhenfeng
    Ren, Liangcai
    2010 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-5, 2010, : 3245 - 3248
  • [27] Optimal Tracking Control of Mini Unmanned Helicopter based Iterative Approximating
    Shang, Yujia
    Lu, Tielin
    PROCEEDINGS OF 2019 IEEE 3RD INFORMATION TECHNOLOGY, NETWORKING, ELECTRONIC AND AUTOMATION CONTROL CONFERENCE (ITNEC 2019), 2019, : 81 - 87
  • [28] Design and Implementation of Ground Monitor and Control System for a Mini Unmanned Helicopter
    Wang, Hui
    Li, Jian
    Hu, Fei
    An, Jie
    2011 INTERNATIONAL CONFERENCE ON COMPUTER SCIENCE AND NETWORK TECHNOLOGY (ICCSNT), VOLS 1-4, 2012, : 2241 - 2246
  • [29] Linear quadratic optimal model-following control of a helicopter in hover
    Pieper, JK
    Baillie, S
    Goheen, KR
    OPTIMAL CONTROL APPLICATIONS & METHODS, 1996, 17 (02): : 123 - 140
  • [30] Linear quadratic optimal model-following control of a helicopter in hover
    Pieper, J.K.
    Baillie, S.
    Goheen, K.R.
    1996, John Wiley & Sons Ltd, Chichester, United Kingdom (17)
12345