JPH0633989Y2 - 模型用レートジャイロ - Google Patents
模型用レートジャイロInfo
- Publication number
- JPH0633989Y2 JPH0633989Y2 JP10448190U JP10448190U JPH0633989Y2 JP H0633989 Y2 JPH0633989 Y2 JP H0633989Y2 JP 10448190 U JP10448190 U JP 10448190U JP 10448190 U JP10448190 U JP 10448190U JP H0633989 Y2 JPH0633989 Y2 JP H0633989Y2
- Authority
- JP
- Japan
- Prior art keywords
- gimbal
- hall sensor
- shaft
- magnet
- rotation angle
- 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.)
- Expired - Lifetime
Links
- 230000004907 flux Effects 0.000 claims description 31
- 230000007935 neutral effect Effects 0.000 claims description 4
- 238000001514 detection method Methods 0.000 description 26
- 230000008859 change Effects 0.000 description 8
- 230000002708 enhancing effect Effects 0.000 description 7
- 230000035945 sensitivity Effects 0.000 description 7
- 230000007423 decrease Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 229910001218 Gallium arsenide Inorganic materials 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003623 enhancer Substances 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- WPYVAWXEWQSOGY-UHFFFAOYSA-N indium antimonide Chemical compound [Sb]#[In] WPYVAWXEWQSOGY-UHFFFAOYSA-N 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Landscapes
- Toys (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10448190U JPH0633989Y2 (ja) | 1990-10-05 | 1990-10-05 | 模型用レートジャイロ |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10448190U JPH0633989Y2 (ja) | 1990-10-05 | 1990-10-05 | 模型用レートジャイロ |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH0461597U JPH0461597U (en]) | 1992-05-27 |
JPH0633989Y2 true JPH0633989Y2 (ja) | 1994-09-07 |
Family
ID=31849774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP10448190U Expired - Lifetime JPH0633989Y2 (ja) | 1990-10-05 | 1990-10-05 | 模型用レートジャイロ |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0633989Y2 (en]) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3455130A4 (en) * | 2016-05-13 | 2020-03-18 | Top Flight Technologies, Inc. | PASSENGER-FREE AIR VEHICLE POWERED BY A HYBRID GENERATOR SYSTEM |
-
1990
- 1990-10-05 JP JP10448190U patent/JPH0633989Y2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH0461597U (en]) | 1992-05-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5386738A (en) | Direct torque control moment gyroscope | |
US4082005A (en) | Spin coupled, angular rate sensitive inertial sensors with mounting structure and method of fabricating and mounting same | |
US4316394A (en) | Magnetically suspended free rotor gyroscope | |
US4285552A (en) | Torquer apparatus for magnetically suspended members | |
US2815584A (en) | Gyro combining limited freedom and angular rate sensitivity | |
US6399941B1 (en) | Inclination angle sensor | |
US4397185A (en) | Inertial instrument with cup-shaped inertial mass | |
US3767139A (en) | Spacecraft spin stabilization system | |
US3858328A (en) | Means and techniques useful in gyros | |
US3490297A (en) | Dual-rotor inertial sensor | |
US3748912A (en) | Gyroscope with universally mounted rotor | |
JPH0633989Y2 (ja) | 模型用レートジャイロ | |
US4114451A (en) | Moving coil miniature angular rate sensor | |
US3974701A (en) | Spin coupled, angular rate sensitive inertial sensors with optional acceleration sensing capability and method of fabricating same | |
JPH0633990Y2 (ja) | 模型用レートジャイロ | |
US4977679A (en) | Azimuth signal generator | |
EP0007583B1 (en) | Change of angular acceleration sensor | |
JPH04212013A (ja) | 角速度検出装置 | |
US5339690A (en) | Apparatus for measuring the rate of rotation and linear accelleration of a moving body in two perpendicular axes | |
US4114452A (en) | Moving magnet miniature angular rate sensor | |
JPH0469729B2 (en]) | ||
US5035376A (en) | Actively damped steering rate sensor for rotating airframe autopilot | |
US3178946A (en) | Rotating pendulum accelerometer | |
US4445375A (en) | Tuned coriolis angular rate measuring device | |
JP2004109059A (ja) | ジャイロの設置方法およびジャイロデバイス |