JPS6163109U - - Google Patents
Info
- Publication number
- JPS6163109U JPS6163109U JP14748284U JP14748284U JPS6163109U JP S6163109 U JPS6163109 U JP S6163109U JP 14748284 U JP14748284 U JP 14748284U JP 14748284 U JP14748284 U JP 14748284U JP S6163109 U JPS6163109 U JP S6163109U
- Authority
- JP
- Japan
- Prior art keywords
- rotation period
- gyroscope
- roll
- angular velocity
- coil
- 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
- 238000001514 detection method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
Landscapes
- Gyroscopes (AREA)
Description
第1図はこの考案の飛しよう体の姿勢角検出装
置の一実施例の構成を示すブロツク図、第2図は
同上飛しよう体の姿勢角検出装置におけるジヤイ
ロとコイルの位置関係を示す図、第3図は同上飛
しよう体の姿勢角検出装置におけるジヤイロの回
転によりコイル両端に発生する電圧波形の一例を
示す図である。
1…ジヤイロ、2…コイル、3…ジヤイロ回転
周期算出部、4…基準回転周期算出部、5…ロー
ル角速度算出部、6…ロール角算出部、7…機体
、7a…ロール軸。
Fig. 1 is a block diagram showing the configuration of one embodiment of the flying body attitude angle detection device of this invention, and Fig. 2 is a diagram showing the positional relationship between the gyroscope and the coil in the flying body attitude angle detection device. FIG. 3 is a diagram showing an example of a voltage waveform generated at both ends of the coil due to the rotation of the gyroscope in the attitude angle detection device for a flying object. DESCRIPTION OF SYMBOLS 1... Gyroscope, 2... Coil, 3... Gyroscope rotation period calculating section, 4... Reference rotation period calculating section, 5... Roll angular velocity calculating section, 6... Roll angle calculating section, 7... Airframe, 7a... Roll axis.
Claims (1)
されたジヤイロと、上記機体に固定され上記ジヤ
イロの回転周期に対応した電圧を検出するコイル
と、このコイルで検出された電圧により上記ジヤ
イロの回転周期を算出する回転周期算出部と、上
記ジヤイロの一定回転周期を算出する基準回転周
期算出部と、上記一定回転周期と上記ジヤイロの
回転周期とから上記機体のロール角速度を算出す
るロール角速度算出部と、このロール角速度を積
分してロール角を求めるロール角算出部とよりな
る飛しよう体の姿勢角検出装置。 A gyroscope is set around the roll axis of the body of the flying body, a coil is fixed to the body and detects a voltage corresponding to the rotation period of the gyroscope, and the rotation period of the gyroscope is determined by the voltage detected by this coil. a reference rotation period calculation section that calculates a constant rotation period of the gyro; and a roll angular velocity calculation section that calculates a roll angular velocity of the aircraft from the constant rotation period and the rotation period of the gyro. , a roll angle calculation unit that integrates the roll angular velocity to obtain the roll angle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14748284U JPS6163109U (en) | 1984-09-29 | 1984-09-29 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14748284U JPS6163109U (en) | 1984-09-29 | 1984-09-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6163109U true JPS6163109U (en) | 1986-04-28 |
Family
ID=30705708
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14748284U Pending JPS6163109U (en) | 1984-09-29 | 1984-09-29 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6163109U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20180013211A (en) * | 2016-07-29 | 2018-02-07 | 주식회사 한화 | Separable rotary type inducing fuse using assistant sensors and a method for orientation estimation the same |
-
1984
- 1984-09-29 JP JP14748284U patent/JPS6163109U/ja active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20180013211A (en) * | 2016-07-29 | 2018-02-07 | 주식회사 한화 | Separable rotary type inducing fuse using assistant sensors and a method for orientation estimation the same |
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