IT1067300B - PROCESS AND PILOTING SYSTEM USING TOTAL ENERGY - Google Patents
PROCESS AND PILOTING SYSTEM USING TOTAL ENERGYInfo
- Publication number
- IT1067300B IT1067300B IT24989/76A IT2498976A IT1067300B IT 1067300 B IT1067300 B IT 1067300B IT 24989/76 A IT24989/76 A IT 24989/76A IT 2498976 A IT2498976 A IT 2498976A IT 1067300 B IT1067300 B IT 1067300B
- Authority
- IT
- Italy
- Prior art keywords
- total energy
- piloting system
- piloting
- total
- energy
- Prior art date
Links
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
-
- 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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7521137A FR2316647A1 (en) | 1975-07-04 | 1975-07-04 | Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity |
FR7537862A FR2334993A2 (en) | 1975-12-10 | 1975-12-10 | Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity |
FR7615929A FR2353090A2 (en) | 1976-05-26 | 1976-05-26 | Aircraft total energy control system - has aerodynamic and selected climb or inclination modulated with respect to deviations in velocity |
Publications (1)
Publication Number | Publication Date |
---|---|
IT1067300B true IT1067300B (en) | 1985-03-16 |
Family
ID=27250494
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT24989/76A IT1067300B (en) | 1975-07-04 | 1976-07-02 | PROCESS AND PILOTING SYSTEM USING TOTAL ENERGY |
Country Status (4)
Country | Link |
---|---|
CA (1) | CA1088655A (en) |
DE (1) | DE2630651A1 (en) |
GB (1) | GB1553407A (en) |
IT (1) | IT1067300B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4609987A (en) * | 1983-03-09 | 1986-09-02 | Safe Flight Instrument Corporation | Aircraft guidance system for take off or go-around during severe wind shear |
US10302451B1 (en) * | 2018-02-20 | 2019-05-28 | The Boeing Company | Optimizing climb performance during takeoff using variable initial pitch angle target |
CN112947520B (en) * | 2021-02-08 | 2023-02-28 | 北京电子工程总体研究所 | Attitude control method and device for improving stability of low-speed aircraft under stall |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1102781A (en) * | 1965-01-20 | 1968-02-07 | Smiths Industries Ltd | Improvements in or relating to aircraft instruments |
US3748980A (en) * | 1971-12-06 | 1973-07-31 | Polaroid Corp | Flash socket assembly |
-
1976
- 1976-06-28 GB GB26757/76A patent/GB1553407A/en not_active Expired
- 1976-07-02 CA CA256,222A patent/CA1088655A/en not_active Expired
- 1976-07-02 IT IT24989/76A patent/IT1067300B/en active
- 1976-07-05 DE DE19762630651 patent/DE2630651A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB1553407A (en) | 1979-09-26 |
CA1088655A (en) | 1980-10-28 |
DE2630651A1 (en) | 1977-01-20 |
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