JPH0387098U - - Google Patents
Info
- Publication number
- JPH0387098U JPH0387098U JP14885889U JP14885889U JPH0387098U JP H0387098 U JPH0387098 U JP H0387098U JP 14885889 U JP14885889 U JP 14885889U JP 14885889 U JP14885889 U JP 14885889U JP H0387098 U JPH0387098 U JP H0387098U
- Authority
- JP
- Japan
- Prior art keywords
- wing
- pitch direction
- limit value
- flying object
- direction steering
- 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
- 206010034719 Personality change Diseases 0.000 claims 1
- 230000002411 adverse Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 5
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図はこの考案の一実施例による飛しよう体
操舵装置の機能ブロツク図、第２図ａ，ｂは飛し
よう体の航空機携行状態を示す図、第３図は飛し
よう体の航空機からの投下状態を示す図、第４図
ａ，ｂは飛しよう体姿勢と操舵翼角との関係を示
す図、第５図は従来の飛しよう体操舵装置の機能
ブロツク図を示す。
Figure 1 is a functional block diagram of a flight control system according to an embodiment of this invention, Figures 2a and b are diagrams showing the state in which the flight body is being carried by an aircraft, and Figure 3 is a diagram showing how the flight body is carried by the aircraft. 4a and 4b are diagrams showing the relationship between the flying body attitude and the steering wing angle, and FIG. 5 is a functional block diagram of a conventional flying gymnastics steering system.
Claims (1)
よう体に固定されている操舵翼がフリー状態にあ
る時に、飛しよう体のピツチ方向姿勢変動がピツ
チ方向操舵翼のフリー可動範囲を越えると、ヨー
方向操舵翼可動範囲のリミツト値を減少させてピ
ツチ方向操舵翼可動範囲のリミツト値を増大させ
、ピツチ方向操舵翼がリミツト値にかかることに
よつて生じる飛しよう体姿勢変動への悪影響を防
止できることを特徴とする飛しよう体操舵装置。 In a flying object dropped from an aircraft, when the control wing fixed to the flying object is in a free state, if the pitch direction attitude change of the flying object exceeds the free movement range of the pitch direction control wing, the yaw direction steering It is characterized by reducing the limit value of the wing movable range and increasing the limit value of the pitch direction steering wing movable range, thereby preventing an adverse effect on the flight body attitude fluctuation caused by the pitch direction steering wing reaching the limit value. Let's fly with the rudder device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14885889U JPH0387098U (en) | 1989-12-25 | 1989-12-25 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14885889U JPH0387098U (en) | 1989-12-25 | 1989-12-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0387098U true JPH0387098U (en) | 1991-09-04 |
Family
ID=31695289
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14885889U Pending JPH0387098U (en) | 1989-12-25 | 1989-12-25 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0387098U (en) |
-
1989
- 1989-12-25 JP JP14885889U patent/JPH0387098U/ja active Pending
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