摘要:
An aircraft simulating apparatus for helicopter hover simulation comprises a cabin (10) containing in its interior a user interface (14) with operating means adapted for simulating flight controls and at least one seat to accommodate a user in a pilot position to operate the flight controls, a carrying portion (20, 30) for supporting and moving the cabin, and a controller (50) adapted to control-movements of the cabin (10) in accordance with a hover simulation characteristics and dependent on the operation of the operating means for simulating flight controls. The carrying portion is adapted to move the cabin along translational movements in three spatial directions (X, Y, Z) and rotational movements around axes in three spatial directions (X, Y, Z), and includes a self-driven support vehicle (30) adapted to perform movement on a ground surface at least along a forward direction (Χ') and around one rotation axis (Ζ') for rotating the forward direction (Χ'), and a robot arm (20) supported by the support vehicle to be moved therewith while holding and supporting the cabin.
摘要:
An aircraft control system for a user of a simulated aircraft. The system includes input devices for controlling the simulated aircraft, a video display having three-dimensional graphics, modeling software for determining position and orientation information based on desired direction of flight obtained through the input devices. User controls desired direction of flight through the input devices, thus controlling aircraft. The aircraft control system may be embodied as a flight game.
摘要:
Die Bewegung von Prüfkörpern entlang beliebiger Trajektorien und mit beliebigen Geschwindigkeiten soll bei Charakterisierung oder Prüfung der Funktion von Fahrerassistenzsystemen ermöglicht werden. Es wird eine Vorrichtung vorgeschlagen, die als Tragseilvorrichtung ausgeführt ist und vier Seile (18), zu jedem Seil jeweils eine elektrisch ansteuerbare Auf- und Abwickeleinrichtung (16) sowie zu jedem Seil (18) jeweils einen Tragmast (14) aufweist. Eine Halteeinrichtung (24) zur Befestigung des Prüfkörpers (12) koppelt die Seile (18). Eine Steuereinrichtung (28) empfängt Positionssignale mit Informationen über die jeweils augenblickliche Position eines Kraftfahrzeugs (32) auf einem Versuchsfeld (10), verarbeitet diese Positionssignale und erzeugt Steuersignale, die eine Bewegung des Prüfkörpers in einer vorbestimmten Weise veranlassen.
摘要:
An aircraft avionics system (10) for an aircraft, comprising a mission system (2), controlled by an open systems mission computer (OSMC) with a tactical communications system (320) and a tactical navigation system (220); a civil system (1), controlled by a flight management system (FMS) with a civil communications system (310) and a civil navigation system (210), wherein said mission system (2) is logically separated from the civil system (1) through separation of a navigation system (20) of the aircraft into civil navigation system (210) and tactical navigation system (220) and through separation of a communications system (30) of the aircraft (100) into said tactical communications system (320) and said civil communications system (310) and through the independence of the open systems mission computer (OSMC) from the flight management system (FMS), said separation allowing the civil system (1) to operate and be updated independently from the mission system (2).
摘要:
In order to save flight time and resources of a flight school, the invention provides a flight school equipment, comprising: at least one data processing device , an aircraft for conducting a real training flight wherein a real flight data ac-quisition device for acquiring real flight data during the real training flight is arranged on the aircraft, at least one student user interface device having a student user interface to be used by a flight student wherein the student user interface device is configured at least for providing information to the student, at least one trainer user interface device having a trainer user interface to be used by a trainer wherein the trainer user interface device is at least configured for providing information to the trainer, at least one student monitoring device for acquiring health and/or movement parameter data of the student during the real training flight.
摘要:
A user interface for a simulated wireless arrangement for communicating audio content in a distributed simulation process being a flight operation and control exercise performed by a plurality of simulation entities (8, 10) each representing a real-world entity from the following entity types: i) vehicles, ii) mission controllers, iii) airspace controllers; comprising: audio input and output means (24, 260) arranged for a human to input and receive output of speech during the distributed simulation process; and simulated wireless control input means (62, 90, 1 10), for use by the human operator to control the simulated wireless arrangement, comprising screen icons (64, 68, 70 72, 74, 76) adapted for the human operator to press, allowing control input related to one or more of: i) push-to-talk; ii) selection between a plurality of simulated wireless channels; iii) selection of respective simulated frequencies for the plurality of simulated wireless channels.
摘要:
Die Bewegung von Prüfkörpern entlang beliebiger Trajektorien und mit beliebigen Geschwindigkeiten soll bei Charakterisierung oder Prüfung der Funktion von Fahrerassistenzsystemen ermöglicht werden. Es wird eine Vorrichtung vorgeschlagen, die als Tragseilvorrichtung ausgeführt ist und vier Seile (18), zu jedem Seil jeweils eine elektrisch ansteuerbare Auf- und Abwickeleinrichtung (16) sowie zu jedem Seil (18) jeweils einen Tragmast (14) aufweist. Eine Halteeinrichtung (24) zur Befestigung des Prüfkörpers (12) koppelt die Seile (18). Eine Steuereinrichtung (28) empfängt Positionssignale mit Informationen über die jeweils augenblickliche Position eines Kraftfahrzeugs (32) auf einem Versuchsfeld (10), verarbeitet diese Positionssignale und erzeugt Steuersignale, die eine Bewegung des Prüfkörpers in einer vorbestimmten Weise veranlassen.
摘要:
A system for evaluating a cyber-attack on an aircraft (138) may include a display (154, 176) associated with the aircraft (138), a sensor system (178) configured to generate sensor data (180) for a pilot (102), and a data processing system (300) configured to: (1) generate simulation data (172), (2) generate a flight simulation (108) from the simulation data (172), (3) simulate the cyber-attack on at least one aircraft system (140) during the flight simulation (108), (4) generate virtual flight data (182) during the flight simulation (108), and (5) present the sensor data (180) and the virtual flight data (182).
摘要:
A system and method for conducting flight procedures training in a rotary-wing aircraft with a multi-engine powerplant includes determining a variable bias relative an available power margin to simulate a reduced power available flight condition; and displaying symbology indicative of the simulated reduced power available flight condition.