DE1302177B - - Google Patents
Info
- Publication number
- DE1302177B DE1302177B DE19651302177D DE1302177DA DE1302177B DE 1302177 B DE1302177 B DE 1302177B DE 19651302177 D DE19651302177 D DE 19651302177D DE 1302177D A DE1302177D A DE 1302177DA DE 1302177 B DE1302177 B DE 1302177B
- Authority
- DE
- Germany
- Prior art keywords
- signal
- aircraft
- angle
- function
- dependent
- 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
- 230000001419 dependent effect Effects 0.000 claims description 17
- 230000001133 acceleration Effects 0.000 claims description 13
- 238000012806 monitoring device Methods 0.000 claims description 11
- 230000008859 change Effects 0.000 claims description 5
- 230000000977 initiatory effect Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 claims description 2
- 230000008569 process Effects 0.000 claims description 2
- 230000003321 amplification Effects 0.000 claims 1
- 230000007257 malfunction Effects 0.000 claims 1
- 238000012544 monitoring process Methods 0.000 claims 1
- 238000003199 nucleic acid amplification method Methods 0.000 claims 1
- 230000009194 climbing Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- 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
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Navigation (AREA)
- Gyroscopes (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB52430/64A GB1131431A (en) | 1964-12-24 | 1964-12-24 | Improvements in or relating to aircraft instruments |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1302177B true DE1302177B (OSRAM) | 1970-07-23 |
Family
ID=10463898
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19651302177D Pending DE1302177B (OSRAM) | 1964-12-24 | 1965-12-23 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3370461A (OSRAM) |
| DE (1) | DE1302177B (OSRAM) |
| FR (1) | FR1469093A (OSRAM) |
| GB (1) | GB1131431A (OSRAM) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1224981A (en) * | 1965-01-20 | 1971-03-10 | Smiths Industries Ltd | Improvements in or relating to aircraft instruments |
| FR2411439A2 (fr) * | 1977-12-06 | 1979-07-06 | Equip Navigation Aerienne | Procede et systeme de pilotage utilisant l'energie totale |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3077109A (en) * | 1959-06-17 | 1963-02-12 | Sperry Rand Corp | Aircraft take-off performance monitoring apparatus |
| US3200642A (en) * | 1962-06-25 | 1965-08-17 | Charles A Neuendorf | Maximum performance take-off director |
| GB1086211A (en) * | 1963-04-19 | 1967-10-04 | Elliott Brothers London Ltd | Director system for aircraft |
-
1964
- 1964-12-24 GB GB52430/64A patent/GB1131431A/en not_active Expired
-
1965
- 1965-12-21 US US515432A patent/US3370461A/en not_active Expired - Lifetime
- 1965-12-23 DE DE19651302177D patent/DE1302177B/de active Pending
- 1965-12-24 FR FR43734A patent/FR1469093A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB1131431A (en) | 1968-10-23 |
| FR1469093A (fr) | 1967-02-10 |
| US3370461A (en) | 1968-02-27 |
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