flight control in Vietnamese

Danh từ
sự kiểm tra tàu bay
hệ thống kiểm tra trên tàu bay

Sentence patterns related to "flight control"

Below are sample sentences containing the word "flight control" from the English - Vietnamese Medical Dictionary. We can refer to these sentence patterns for sentences in case of finding sample sentences with the word "flight control", or refer to the context using the word "flight control" in the English - Vietnamese Medical Dictionary.

1. "Flight control optical sensor array" specially designed for implementing "active flight control systems"; b.

2. Airframe – Materials – Flight control system

3. I have an emergency flight control malfunction.

Tôi bị hỏng chức năng điều khiển bay khẩn cấp.

4. Level flight, control of heading, altitude/height and speed

5. In this configuration, the flight control systems must simulate "feel".

Ở cấu hình này, các hệ thống điều khiển bay phải tái tạo sự "cảm nhận".

6. 4. Fault-tolerant or self-reconfiguring "active flight control systems";

7. Aerial view of the area surrounding the Flight Control Tower.

8. Level flight, control of heading, altitude and airspeed, power setting, trim technique

9. Nellis Tower, this is Tasty 1-1 with an emergency flight control malfunction.

10. In detail, it comprises an airframe (11) having aerodynamic lift and flight control surfaces.

11. 11.3.4 Flight Control Surfaces (ATA 55/57) Construction and attachment; Balancing — mass and aerodynamic.

12. ‘Inner-loop’ refers to functions of “active flight control systems” that automate airframe stability controls.

13. 'Inner-loop' refers to functions of "active flight control systems" that automate airframe stability controls.

14. The characteristics of an aircraft flight control system have a major effect on the handling qualities.

15. Republic received an additional contract to continue the experiments by incorporating an automatic flight control system.

Republic nhận được 1 hợp đồng bổ sung để tiếp tục nghiên cứu cách kết hợp một hệ thống điều khiển bay tự động.

16. “Modern aircraft rely on both sophisticated flight control systems and advanced integrated mission systems for their effectiveness.

17. "Development""technology", as follows, for "active flight control systems" (including fly-by-wire or fly-by-light):

18. Ailerons are a primary flight control surface which control movement about the longitudinal axis of an aircraft

19. No. 71-0290) The F-15 ACTIVE was then converted into an intelligent flight control systems research aircraft.

20. These tests were followed with three test flights with Enterprise manned to test the shuttle flight control systems.

Sau đó, Enterprise được bay ba lần với người lái, để thử các hệ thống điều khiển bay.

21. The Shuttle was one of the earliest craft to use a computerized fly-by-wire digital flight control system.

Tàu con thoi là một trong những phi thuyền đầu tiên sử dụng hệ thống điều khiển bay tự động bằng máy tính fly-by-wire.

22. While the Buzzbomb echoes the lines of the championship wining predecessor, the construction, styling, and flight control is refreshingly modern.

23. With hydraulic flight control systems, the aircraft's size and performance are limited by economics rather than a pilot's muscular strength.

Với các hệ thống điều khiển bay thuỷ lực, kích thước và tính năng của máy bay bị hạn chế bởi tính kinh tế chứ không phải ở sức khoẻ của phi công nữa.

24. Currently research is done on the carrier rocket Hercules III , the flight control system Robolaunch and the aero dynamics simulation ViWiAn.

25. 'Primary flight control' is "aircraft" stability or manoeuvring control using force/moment generators, i.e. aerodynamic control surfaces or propulsive thrust vectoring.

26. First, project partners looked at various aerodynamic derivatives of relevance to flight control systems, i.e. measures of how particular forces affect aircraft stability.

27. ‘Primary flight control’ (7) means an ‘aircraft’ stability or manoeuvering control using force/moment generators, i.e., aerodynamic control surfaces or propulsive thrust vectoring.

28. These facilities make it possible to conduct experiments in man-machine factors, flight control, structures and materials, aerodynamics, simulation, motion, navigation and spaceflight.

29. The ground experiment's result about the semi-physical simulation shows that triplex Hot-redundancy flight control computer's communication system design is rational, feasible and reliable.

30. Flight Control The heart of the LCA , it uses advanced digital fly - by - wire technology which essentially employs computers to optimise the aircraft ' s performance .

31. Archer's world-class team is focused on vertically integrating key enabling technologies including aircraft design, electric powertrain, and avionics and flight control software to revolutionize air travel.

32. It incorporates a number of advanced technologies; Integrated Dynamic System (IDS), Anti-resonance Isolation System (ARIS), Full Authority Digital Electronic Control (FADEC), Hingeless Main Rotor, Bearingless Tail Rotor, and Automatic Flight Control System.

33. The digital FBW system of the aircraft employs an advance next-generation distributed digital flight control computer (DDFCC) made by ADE comprising four computing channels, each with its own independent power supply and all housed in differently placed LRU.

34. The next-generation Genesys Aerosystems S-TEC 3100 Digital Flight Control System (DFCS) is a fully-featured, attitude-based autopilot that gives you a list of workload-reducing and safety-enhancing capabilities that were previously unavailable on aftermarket Autopilots.

35. (1) The parameters necessary to determine altitude, airspeed, heading, acceleration, pitch and roll attitude, radio transmission keying, thrust or power on each engine, configuration of lift and drag devices, air temperature, use of automatic flight control systems and angle of attack;

36. Known flying objects (01) are controlled independently at the flying height by means of an automatic flight control system and have an adjustment device of the aerofoils which is retracted into the non-deflected home position in the event of malfunctions occurring.

37. Whenever, as a result of failure or degradation of navigation, communications, altimetry, flight control or other systems, aircraft performance is degraded below the level required for the airspace in which it is operating, the flight crew shall advise the ATC unit concerned without delay.

38. Chromate conversion coatings are used for heat sinks, automotive wheels, and everyday aluminum hardware and components. In aerospace applications, Chromate conversion coatings are used on aircraft hulls, including shock absorbers, side and torsion struts, landing gear, and flight control systems such as rudder systems and wing parts.

39. Combining outstanding reliability with silky-smooth servo inputs and a full range of workload-reducing modes, functions and self-monitoring features, Garmin digital Autopilot systems — available for retrofit or forward-fit installations — bring the latest in safety-enhancing flight control solutions to a broad spectrum of certified and experimental aircraft.

40. In a manned spacecraft, Avionics refers to all the electronics-based instrumentation that enables essential capabilities such as communication, navigation, flight control (FC), data handling (DH), and vehicle management for the MSA ; therefore, as the Avionics’ health condition and effectiveness directly influence manned space flight safety and mission success, an accurate assessment of both the Avionics’ …

41. Canted vertical stabilizers are another distinguishing design element, one among several other such elements that enable the Hornet's excellent high angle of attack ability, including oversized horizontal stabilators, oversized trailing-edge flaps that operate as flaperons, large full-length leading-edge slats, and flight control computer programming that multiplies the movement of each control surface at low speeds and moves the vertical rudders inboard instead of simply left and right.

Các bộ thăng bằng dọc nghiêng là một đặc điểm phân biệt thiết kế khác, một trong nhiều yếu tố khác cho phép Hornet có khả năng đạt góc tấn xuất sắc gồm các bộ ổn định n gang ngoại cỡ, các cánh tà đuôi lái lớn hoạt động như những cánh lái phối hợp, các cánh lái phía trước chạy suốt chiều dài cánh, và chương trình máy tính điều khiển bay điều khiển tăng sự di động của mỗi bề mặt điều khiển ở những tốc độ thấp và di chuyển các đuôi lái ở trong thay vì chỉ đơn giản di chuyển trái và phải.