摘要:
Digital recording and replay system for an aircraft, comprising a Mission Computer with an Operational Flight Program for generating instrument data for onboard instruments of the aircraft; a Mission Data Recorder connected to said Mission Computer for recording said instrument data; and a Mission Debriefing System; wherein the Mission Debriefing System is configured to reproduce the onboard instruments of the aircraft based on instrument data retrieved from the Mission Data Recorder. Method for reproduction of onboard instrumentation of an aircraft, comprising the steps of connecting a Mission Data Recorder to a Mission Computer of an aircraft having an Operational Flight Program for generating instrument data for onboard instruments; recording instrument data; providing a Mission Debrief System and causing it to reproduce the onboard instruments of the aircraft based on instrument data retrieved from the Mission Data Recorder.
摘要:
Training method for the simulation of an operation performed by at least one device which is part of a real apparatus, wherein the method comprises providing to display means overlaid images under controlled depth order of a virtual apparatus, and real images of said device, and providing a simulated response to control means, based on data of the position and behavior of said device and on data of the position and behavior of said virtual apparatus.
摘要:
A vehicle pneumatic system training aid comprises simulated controls and indicators and a pneumatic circuit. The simulated controls and indicators correspond to at least a portion of controls and indicators on an actual vehicle. The pneumatic circuit comprises a connection to a source of pressurized fluid, and at least one fluid flow control device. The fluid flow control device is positionable in at least two different positions corresponding to different actual vehicle conditions that are simulatable. The simulated controls are actuatable to change a condition of the pneumatic circuit and the simulated indicators are operable to display an indication of the condition of the pneumatic circuit.
摘要:
A method and apparatus for training in an aircraft. A display system is associated with an aircraft. A sensor system is associated with the aircraft. A training processor is configured to be connected to the aircraft. The training processor is configured generate constructive data for a number of simulation objects and generate simulation sensor data using the constructive data. The training processor is further configured to present the simulation sensor data with live sensor data generated by the sensor system for an aircraft on a display system in the aircraft.
摘要:
A method and apparatus for a uniform resolution display screen. In one embodiment, the uniform resolution display screen comprises a surface of the uniform resolution display screen having a curvature configured to display images with a uniform resolution across the display screen. The curvature is based on a projection distance from a projector to the uniform resolution display screen and a viewing distance from an eyepoint of an observer to the uniform resolution display screen. The geometry of the display screen is configured to display images associated with a high definition imaging format.
摘要:
The present invention provides computer implemented methodology that permits the safe landing and recovery of rotorcraft following engine failure. With this invention successful autorotations may be performed from well within the unsafe operating area of the height-velocity profile of a helicopter by employing the fast and robust real-time trajectory optimization algorithm that commands control motion through an intuitive pilot display, or directly in the case of autonomous rotorcraft. The algorithm generates optimal trajectories and control commands via the direct-collocation optimization method, solved using a nonlinear programming problem solver. The control inputs computed are collective pitch and aircraft pitch, which are easily tracked and manipulated by the pilot or converted to control actuator commands for automated operation during autorotation in the case of an autonomous rotorcraft. The formulation of the optimal control problem has been carefully tailored so the solutions resemble those of an expert pilot, accounting for the performance limitations of the rotorcraft and safety concerns.
摘要:
A simulator is disclosed which includes an image generator that includes a forward display system and a peripheral display system to provide a field of view. The forward display system utilizes a forward projection system to provide forward imagery with high-resolution. The peripheral display system utilizes a helmet-mounted display system to provide peripheral imagery. The forward and peripheral imagery are merged by the image-generator so as to provide a full field of view with as much high-resolution imagery as possible.
摘要:
Systems and methods for use in training observers and search and rescue personnel in detecting and identifying visual cues related to potential threats to aircraft and to ground based search and rescue circumstances. A visual display displays a scene generated by a visual scene generator apparatus. A vision limiting device is placed between the trainee and the visual display and the trainee can only see a limited amount of the visual display through a window on the vision limiting device. The limited view of the scene afforded the trainee will force the trainee to move around at various angles to see more of the scene as he normally would in real life.
摘要:
An interchangeable instrument panel, throttle quadrant, and control device (stick and/or yoke) for a flight simulation system each independently interchangeable with another simulating a different aircraft. Each instrument panel simulating a particular type of aircraft and containing switches, knobs, and/or buttons of approximately the same type and approximately the same location as in the simulated aircraft. The instrument panels capable of simulating a variety of avionics suites, gauges, and other equipment. Each throttle quadrant simulating a particular type of aircraft (e.g. single engine; multi-engine; knob/pull style; lever style).