FR1074753A - Complementary system for radio-guided aircraft landing - Google Patents
Complementary system for radio-guided aircraft landingInfo
- Publication number
- FR1074753A FR1074753A FR1074753DA FR1074753A FR 1074753 A FR1074753 A FR 1074753A FR 1074753D A FR1074753D A FR 1074753DA FR 1074753 A FR1074753 A FR 1074753A
- Authority
- FR
- France
- Prior art keywords
- radio
- aircraft landing
- complementary system
- guided aircraft
- guided
- 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.)
- Expired
Links
- 230000000295 complement effect Effects 0.000 title 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
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1074753XA | 1952-01-15 | 1952-01-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1074753A true FR1074753A (en) | 1954-10-08 |
Family
ID=22316802
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1074753D Expired FR1074753A (en) | 1952-01-15 | 1953-01-12 | Complementary system for radio-guided aircraft landing |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE975456C (en) |
FR (1) | FR1074753A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1236346B (en) * | 1959-07-07 | 1967-03-09 | Cutler Hammer Inc | Device for guiding aircraft on an interception runway |
DE1291637B (en) * | 1962-03-30 | 1969-03-27 | North American Aviation Inc | Automatic longitudinal inclination control device for airplanes and unmanned aerial vehicles for carrying out the landing approach on a given landing approach path |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE687316C (en) * | 1937-12-05 | 1940-01-26 | Versuchsanstalt Fuer Luftfahrt | Process for generating a straight glide path for blind landing of aircraft |
DE716679C (en) * | 1939-04-07 | 1942-01-26 | Telefunken Gmbh | Procedure for displaying the altitude of an aircraft during the landing process |
US2507304A (en) * | 1944-07-25 | 1950-05-09 | Norden Lab Corp | Altitude control for aircraft |
-
1953
- 1953-01-11 DE DES31784A patent/DE975456C/en not_active Expired
- 1953-01-12 FR FR1074753D patent/FR1074753A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE975456C (en) | 1961-11-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR1050166A (en) | Linkage system | |
FR1074753A (en) | Complementary system for radio-guided aircraft landing | |
FR1128574A (en) | Machining device | |
FR1062307A (en) | Suspension device in particular for vehicles | |
FR1049955A (en) | Device for braking landing planes | |
FR1071458A (en) | Device for frequency comparison | |
FR1097660A (en) | Aircraft braking mechanism | |
FR1080832A (en) | Device for landing, take-off and landing of airplanes | |
FR1059996A (en) | Device for air defense carriages | |
FR1082593A (en) | Fuze for aviation grenade | |
FR1063884A (en) | Universal post system for demountable constructions | |
FR1062444A (en) | Advanced aircraft jack | |
FR1079341A (en) | Aircraft safety device | |
FR1079836A (en) | Aircraft braking device | |
FR1076863A (en) | Aircraft fuselage | |
FR1102295A (en) | Landing process for airplanes | |
FR1053430A (en) | Tourist seat for aircraft | |
FR1047826A (en) | Aircraft braking system | |
FR1090929A (en) | Pylon for air carriers | |
FR1058373A (en) | Parachutist harness | |
FR1051994A (en) | Removable bottle stopper | |
FR1076324A (en) | Parachutist | |
FR1076744A (en) | Device for the production of electric flashes | |
FR1079645A (en) | Separating agent for filters | |
FR1084936A (en) | Elastic hub for aviation propellers |