FR1549195A - - Google Patents
Info
- Publication number
- FR1549195A FR1549195A FR1549195DA FR1549195A FR 1549195 A FR1549195 A FR 1549195A FR 1549195D A FR1549195D A FR 1549195DA FR 1549195 A FR1549195 A FR 1549195A
- Authority
- FR
- France
- 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
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
- G05D1/0638—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by combined action on the pitch and on the motors
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEF0049575 | 1966-06-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1549195A true FR1549195A (fr) | 1968-12-13 |
Family
ID=7103120
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1549195D Expired FR1549195A (fr) | 1966-06-29 | 1967-03-08 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3533579A (fr) |
DE (1) | DE1481548C3 (fr) |
FR (1) | FR1549195A (fr) |
GB (1) | GB1190198A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2435392A1 (fr) * | 1978-09-11 | 1980-04-04 | Lockheed Corp | Systeme de commande de la vitesse de croisiere d'un avion |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3624364A (en) * | 1970-01-28 | 1971-11-30 | Us Army | Parallel speed stabilization system |
US4325123A (en) * | 1978-07-28 | 1982-04-13 | The Boeing Company | Economy performance data avionic system |
US4490793A (en) * | 1981-12-21 | 1984-12-25 | Sperry Corporation | Cruise speed control for aircraft performance management system |
GB2237899B (en) * | 1989-11-10 | 1994-05-11 | Fokker Aircraft Bv | Automated approach speed control for an airplane |
US7031811B2 (en) * | 2003-05-30 | 2006-04-18 | The Boeing Company | Fuel efficient airspeed trim |
CN109460052B (zh) * | 2019-01-09 | 2022-08-05 | 翁雷 | 一种可拼组飞行器的控制方法 |
CN109782806B (zh) * | 2019-02-19 | 2020-10-23 | 北京邮电大学 | 一种无人机室内路径跟踪方法及装置 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2875965A (en) * | 1954-06-18 | 1959-03-03 | Collins Radio Co | Automatic flight control system |
US2948496A (en) * | 1957-01-09 | 1960-08-09 | Sperry Rand Corp | Speed controlling system for aircraft |
US2932472A (en) * | 1957-09-11 | 1960-04-12 | Gen Electric | Automatic turn compensator for aircraft |
-
1966
- 1966-06-29 DE DE1481548A patent/DE1481548C3/de not_active Expired
-
1967
- 1967-03-08 FR FR1549195D patent/FR1549195A/fr not_active Expired
- 1967-06-21 US US647739A patent/US3533579A/en not_active Expired - Lifetime
- 1967-06-28 GB GB29794/67A patent/GB1190198A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2435392A1 (fr) * | 1978-09-11 | 1980-04-04 | Lockheed Corp | Systeme de commande de la vitesse de croisiere d'un avion |
Also Published As
Publication number | Publication date |
---|---|
DE1481548A1 (de) | 1969-11-06 |
DE1481548C3 (de) | 1975-04-17 |
US3533579A (en) | 1970-10-13 |
GB1190198A (en) | 1970-04-29 |
DE1481548B2 (de) | 1974-08-29 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |