CN103344243B - A kind of aerial remote sensing inertial-stabilized platform friction parameter discrimination method - Google Patents
A kind of aerial remote sensing inertial-stabilized platform friction parameter discrimination method Download PDFInfo
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JP5996127B2 (en) * | 2013-12-06 | 2016-09-21 | 三菱電機株式会社 | Friction identification method and friction identification apparatus |
TW201600846A (en) * | 2014-06-26 | 2016-01-01 | Hiwin Tech Corp | Friction parameter authentication method for linear motion platform |
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CN116175567B (en) * | 2023-02-14 | 2023-11-24 | 合肥合滨智能机器人有限公司 | Identification method for mechanical arm joint friction model parameters and kinetic parameters |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2112926C1 (en) * | 1996-10-28 | 1998-06-10 | Научно-производственный комплекс "Электрооптика" | Method determining spatial angular orientation of mobile object and laser measurement unit |
RU2282153C1 (en) * | 2005-04-12 | 2006-08-20 | Открытое акционерное общество "Раменское приборостроительное конструкторское бюро" | Method of enhancing vibration stability of inertia platform |
CN101709975A (en) * | 2009-11-27 | 2010-05-19 | 北京航空航天大学 | Estimation and compensation method for unbalanced moment of aerial remote sensing inertially stabilized platform |
CN102109350A (en) * | 2010-11-29 | 2011-06-29 | 北京航空航天大学 | Damping method for forced vibration of inertially stabilized platform |
CN102230801A (en) * | 2011-03-30 | 2011-11-02 | 北京航空航天大学 | Light-type triaxial ISP (inertially stabilized platform) system using aerial remote sensing technology |
CN102508503A (en) * | 2011-11-01 | 2012-06-20 | 北京航空航天大学 | Compensation method based on generalized inner module for eccentric torque of three-shaft inertially stabilized platform |
-
2013
- 2013-07-02 CN CN201310275237.6A patent/CN103344243B/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2112926C1 (en) * | 1996-10-28 | 1998-06-10 | Научно-производственный комплекс "Электрооптика" | Method determining spatial angular orientation of mobile object and laser measurement unit |
RU2282153C1 (en) * | 2005-04-12 | 2006-08-20 | Открытое акционерное общество "Раменское приборостроительное конструкторское бюро" | Method of enhancing vibration stability of inertia platform |
CN101709975A (en) * | 2009-11-27 | 2010-05-19 | 北京航空航天大学 | Estimation and compensation method for unbalanced moment of aerial remote sensing inertially stabilized platform |
CN102109350A (en) * | 2010-11-29 | 2011-06-29 | 北京航空航天大学 | Damping method for forced vibration of inertially stabilized platform |
CN102230801A (en) * | 2011-03-30 | 2011-11-02 | 北京航空航天大学 | Light-type triaxial ISP (inertially stabilized platform) system using aerial remote sensing technology |
CN102508503A (en) * | 2011-11-01 | 2012-06-20 | 北京航空航天大学 | Compensation method based on generalized inner module for eccentric torque of three-shaft inertially stabilized platform |
Non-Patent Citations (2)
Title |
---|
基于PID的航空遥感三轴惯性稳定平台控制***设计;李树胜等;《吉林大学学报(工业版)》;20110731;第41卷;全文 * |
航空摄影惯性稳定平台框架动力学研究与分析;周向阳等;《测绘科学》;20130531;第38卷(第3期);全文 * |
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