NL6914824A - - Google Patents
Info
- Publication number
- NL6914824A NL6914824A NL6914824A NL6914824A NL6914824A NL 6914824 A NL6914824 A NL 6914824A NL 6914824 A NL6914824 A NL 6914824A NL 6914824 A NL6914824 A NL 6914824A NL 6914824 A NL6914824 A NL 6914824A
- Authority
- NL
- Netherlands
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/166—Mechanical, construction or arrangement details of inertial navigation systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5875968A GB1279098A (en) | 1968-10-01 | 1968-10-01 | Improvements in orbiting spacecraft or satellite attitude control systems |
| GB4660868 | 1968-10-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL6914824A true NL6914824A (en) | 1970-04-03 |
Family
ID=26265857
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL6914824A NL6914824A (en) | 1968-10-01 | 1969-10-01 |
Country Status (4)
| Country | Link |
|---|---|
| BE (1) | BE739696A (en) |
| DE (1) | DE1950332A1 (en) |
| FR (1) | FR2023313B1 (en) |
| NL (1) | NL6914824A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3834653A (en) * | 1972-03-27 | 1974-09-10 | Rca Corp | Closed loop roll and yaw control for satellites |
| US3937423A (en) * | 1974-01-25 | 1976-02-10 | Hughes Aircraft Company | Nutation and roll error angle correction means |
| CA1073988A (en) * | 1975-07-21 | 1980-03-18 | Ludwig Muhlfelder | Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits |
-
1969
- 1969-10-01 NL NL6914824A patent/NL6914824A/xx unknown
- 1969-10-01 DE DE19691950332 patent/DE1950332A1/en active Pending
- 1969-10-01 FR FR696933480A patent/FR2023313B1/fr not_active Expired
- 1969-10-01 BE BE739696D patent/BE739696A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| FR2023313B1 (en) | 1974-02-22 |
| BE739696A (en) | 1970-03-16 |
| FR2023313A1 (en) | 1970-08-21 |
| DE1950332A1 (en) | 1970-06-11 |