JPS56162106A - Rotatable body driving device - Google Patents
Rotatable body driving deviceInfo
- Publication number
- JPS56162106A JPS56162106A JP6588480A JP6588480A JPS56162106A JP S56162106 A JPS56162106 A JP S56162106A JP 6588480 A JP6588480 A JP 6588480A JP 6588480 A JP6588480 A JP 6588480A JP S56162106 A JPS56162106 A JP S56162106A
- Authority
- JP
- Japan
- Prior art keywords
- angle
- launching pad
- rotatable body
- rotary moment
- rotary
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000005484 gravity Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/12—Target-seeking control
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Control Of Position Or Direction (AREA)
Abstract
PURPOSE:To correct a rotary angle error and to make an angle control system which requires accuracy, small-sized by providing the driving force corresponding to rotary moment by gravity of a rotatable body, to the rotatable body by the second driving part which has been installed separately, in the driving device of a rotatable body whose rotation is driven by a prescribed angle. CONSTITUTION:When the mass W angle alpha , and length of segment L of a launching pad 51 are constants, and also a flying body 52 has all equal mass and always is set at the same position of the launching pad 51, the mass Wk, angle alphak, and length of segment Lk are constants, as well. In this case, the rotary moment Mt becomes a function of only the angle theta and the number of flying bodies 52. Accordingly, an operation part 47 is able to calculate the rotary moment M1 by obtaining the information of the existing angle theta of the launching pad 51 and the information of the number of flying bodies 52 from an angle detector 44 and a load detector 46, respectively. And, the second driving part 48 gives to a launching pad 44 the driving force corresponding to the rotary moment Mt which has been calculated, and corrects an angle error which is caused by the rotary moment Mt of the launching pad 44.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6588480A JPS56162106A (en) | 1980-05-20 | 1980-05-20 | Rotatable body driving device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6588480A JPS56162106A (en) | 1980-05-20 | 1980-05-20 | Rotatable body driving device |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS56162106A true JPS56162106A (en) | 1981-12-12 |
Family
ID=13299841
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP6588480A Pending JPS56162106A (en) | 1980-05-20 | 1980-05-20 | Rotatable body driving device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS56162106A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59163798U (en) * | 1983-04-20 | 1984-11-02 | 三菱重工業株式会社 | rocket launch equipment |
JPS62131298U (en) * | 1986-02-13 | 1987-08-19 | ||
KR100372813B1 (en) * | 2000-11-01 | 2003-02-25 | 한국항공우주연구원 | Mass properties measurement auxiliary fixture with adjustable inclined angle |
KR100422424B1 (en) * | 2001-07-03 | 2004-03-12 | 한국항공우주연구원 | a |
-
1980
- 1980-05-20 JP JP6588480A patent/JPS56162106A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59163798U (en) * | 1983-04-20 | 1984-11-02 | 三菱重工業株式会社 | rocket launch equipment |
JPH0229440Y2 (en) * | 1983-04-20 | 1990-08-07 | ||
JPS62131298U (en) * | 1986-02-13 | 1987-08-19 | ||
JPH0518637Y2 (en) * | 1986-02-13 | 1993-05-18 | ||
KR100372813B1 (en) * | 2000-11-01 | 2003-02-25 | 한국항공우주연구원 | Mass properties measurement auxiliary fixture with adjustable inclined angle |
KR100422424B1 (en) * | 2001-07-03 | 2004-03-12 | 한국항공우주연구원 | a |
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