Abstract: This disclosure describes novel aircraft control systems for propeller-driven training aircraft, and methods for their use. In an aspect of some embodiments, a control system might comprise an integrated power control that takes a single power input from the pilot and translates that input into controls for a throttle, a propeller pitch setting, and a fuel/air mixture. In another aspect of some embodiments, a glass cockpit may be provided, with computer displays emulating the instruments of the aircraft for which the pilot is training. Advantageously, this allows a pilot in training to learn, from the beginning, the power controls and/or instrumentation for the aircraft for which the pilot is training, instead of having to learn one power control and instrumentation system, only to later have to learn another system. In a specific embodiment, the instrumentation displays may be reconfigurable, allowing the displays to emulate those of a variety of jet aircraft.

Abstract: This disclosure describes novel systems, methods and software for providing flight training. In an aspect of some embodiments, flight data is collected during a training flight. That flight data then can be used to provide a review and/or simulation of the training flight. The student may be allowed to participate in the simulation by providing input from a set of controls. In some cases, an instructor (or another) might provide modified flight data, which can be used to modify the simulation. Advantageously, this allows for the analysis and simulation of a variety of hypothetical, “what-if” scenarios.

Abstract: A smoke simulator system (1) for an aircraft simulator cockpit said system (1) comprising a water tank (2), an ultrasonic generator (3), said ultrasonic generator (3) being inside said water tank (2), supply means (7) to said water tank (2) and outlet means (8) from said water tank (2) for smoke. The invention relates as well to a method to operate such a smoke simulator system (1) for an aircraft simulator cockpit.

Abstract: One of the challenges for airports is to provide effective emergency response training in the event of aircraft emergency scenarios. For airports there is the additional expense to provide that training that is typically performed at a remote facility. A portable inflatable training aircraft will provide this training and reduces the cost to the airport management so that the training can be ongoing and effective without interfering with the normal operation of the airport.

Abstract: A method and apparatus for simulating a missile. A simulation program for a weapon using a processor unit is executed in a simulation unit. A number of input signals is received from a control station in a vehicle through an interface system connected to a weapons interface on the vehicle. The interface system is in communications with the processor unit. The control station is capable of operating the weapon connected to the weapons interface. A number of output signals is generated using a simulation of the weapon. The number of output signals is sent through the weapons interface to the control station.

Abstract: The channel assignment data is generated by assigning a channel of the radio control transmitter for the trainee 1B associated with the same controlled object to a channel of the radio control transmitter for the trainer 1A, and stored in the radio control transmitter for the trainer 1A. The radio control transmitter for the trainer 1A converts the channel of the received trainer signal into the steering signal according to the channel assignment data, and transmits the steering signal.

Abstract: A method and apparatus for managing a simulation. Information about the simulation is received over a wireless communications link with a computer system in an aircraft. The information is received during running of the simulation and identifies a performance of the computer system running the simulation. The running of the simulation is controlled based on the performance of the computer system.

Abstract: A system automatically generates a training lesson from a plurality of frames located within the storage. Each frame has a component of training. After operator-related data is collected from one or more vehicles, details of the operator-related data are saved. In some examples, the operator-related data correlates to a single operator (e.g. the driver, pilot, etc. that operated a known vehicle) while in other examples, the operator-related data correlates to several operators. Software selects at least one frame from the plurality of frames based upon the operator-related data and creates a lesson. The lesson, which includes the selected frame(s) from the plurality of frames, is provided to the operator or operators.

Abstract: A flight simulator rests on a plurality of air cushions as a hovercraft and assumes spatial attitudes depending upon the relative heights of the air cushions. Flight controls determine the volume of air supplied to each air cushion and thereby control the pitch and roll attitudes of the flight simulator. The simulator may be connected to an external support frame and may thereby be subjected to longitudinal, lateral, and rotational movements.

Abstract: The invention is embodied in the form of a flight simulator in the conditions of vortex danger and in conditions when a pilot is informed about the possibility to penetrate into said dangerous area of vortex sheddings produced by a vortex generator.

Abstract: A system and device is provided for formulating alerts of the items of equipment of an aircraft. The device includes a database of virtual objects representing the items of equipment for constructing a virtual model representative on the one hand of the topological configuration of the network of items of equipment and on the other hand of the configuration of the chain of functional applications implemented by the items of equipment, means for each virtual object to formulate a request for consulting the status of the functional application carried out by the item of equipment associated with the object and means for detecting alerts for formulating requests for consulting the status of each of the objects of the virtual model so as to detect anomalies of configuration of the topology of the network of items of equipment and of the chain of functional applications of the virtual model and to transmit the alerts associated with the anomalies. The device detects and manages the alerts of an aircraft.

Abstract: The present invention is related to a motion platform and aircraft simulator comprising the same. According to the invention, a motion platform is provided using at least three uprights and a sub-frame connected to the uprights by connecting members. A cabin in which a person can be accommodated is connected to the sub-frame. By restricting the way the various components are capable of moving relative to each other a motion platform is obtained which is able to offer the desired simulation of motion such as translational movement, pitch, roll, and yaw of the cabin.

Abstract: An actuated support frame for transmitting motion to a seat with respect to a ground as a function of motion signals associated with video output, comprises a frame. The frame is expandable/retractable along translational degrees of freedom. Support surfaces are provided on the frame. The support surfaces are displaceable with respect to one another by expansion/retraction of the frame so as to be sized to support a seat. Actuators are provided between the frame and the ground. The actuators receive signals and selectively displace the frame with respect to the ground in synchronization with a video output, whereby a seat supported on the frame is displaceable within the frame. A method for installing a seating system of a motion simulator system is also provided.

Abstract: Systems and methods for use in training crewmembers in the cargo compartment 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, such as an actual door from an aircraft, equipped with a window is placed between the trainee and the visual display and the trainee can only see a limited amount of the visual display through the door's window. 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 and will also provide a frame of reference for making spatiotemporal judgments regarding the relationships between the trainee, the trainee's aircraft, and objects external to the aircraft.

Abstract: A vehicle simulation system equipped to display information on the rear side of a driver (rider). The simulation system includes a dummy bicycle operated by the rider, a monitor on the front side for displaying a scene based on the operations of the dummy bicycle, and a lamp unit connected to the dummy bicycle and provided on the rear side relative to the seated position of the rider. The lamp unit has a red lamp, a yellow lamp and a green lamp, and is controlledly turned ON under the action of a main control unit. An input device is provided on a steering handle of the dummy bicycle. The input device has a switch for red, a switch for yellow, and a switch for green. The rider checks behind, and operates the input device according to the ON/OFF conditions of the lamp unit.

Abstract: An activity device including an activity sensor for generating an activity interaction signal responsive to a sustained large-muscle physical activity of a user operating the activity device; a controller, coupled to the activity monitor, generating a virtual environment supporting a virtual user frame-of-reference in the virtual environment, the controller generating a set of virtual education elements in the environment and a goal for the set virtual representation with respect to the virtual education elements wherein the controller is responsive to the activity interaction signal to produce an affected interaction of the virtual representation with the virtual education elements with the controller measuring a conformation of the goal by the affected interaction; and a feedback system, coupled to the controller, for presenting the virtual environment with the frame-of-reference in relation to the virtual education elements for providing the user with feedback.

Abstract: A system includes a plurality of flight simulators provided with a plurality of control posts and at least one display, wherein at least one control post is movable from a first fixed station to a mobile station.

Abstract: The invention relates to a method to control the movements of a flight simulator involving linear and angular accelerations perceived at a pilot's seat and involving mathematical transformations of a lateral position y and a roll angle ? for said accelerations, wherein mathematical transformations are used with at least one of the following corrections: —Feed-forward of a specific force error due to the y-position wash-out into a roll angle transformation function; —Decomposition of specific force at pilot's position and addition of complementary filters to reproduce suitable side forces in the pilot's seat due to lateral accelerations; —Mathematical transformations linking a pilot's position in an aircraft and flight simulator to a motion base centroid.

Abstract: A method of inspecting an aircraft. A plurality of heterogeneous unmanned vehicles are used to perform an inspection of the aircraft, each unmanned vehicle having one or more sensors. A plurality of portions of the aircraft are assigned to the vehicles for inspection based on functional capability of each vehicle. The unmanned vehicles are configured to cooperatively use the sensors to perform the inspection.

Abstract: A method of performing a flight simulation is provided. The method includes retrieving a flight action, mapping the flight action to an instruction, the instruction being is configured to bring about a desired state of a flight simulator, identifying a command based on the desired state of the flight simulator and a first state of the flight simulator, and determining if a second state of the flight simulator after executing the command matches the desired state of the flight simulator.

Abstract: 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.

Abstract: The invention relates to a tool (10) for assisting in the design of an aircraft flight deck compatible with a night vision system, comprising a closed chamber (12) functioning as a dark room and containing: a mockup (14) that reproduces the interior of a flight deck and is representative of the visual characteristics of the station, the mockup integrating equipment items that are representative of a flight deck and that are capable of reproducing a plurality of possible illumination configurations of the flight deck on command, a light source (22) capable of reproducing at least one level of darkness in the chamber.

Abstract: 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.

Abstract: Disclosed is an aircraft maintenance training system to permit a student to simulate testing, repairing and maintaining components of an aircraft, the system comprising a database of components of the aircraft, an aircraft maintenance display to display a three-dimensional representation of the aircraft, a virtual cockpit display to display a representation of the controls of the aircraft and a processor to simulate operations of the components of the aircraft and allow the student to attach and remove components from the aircraft, and interface support equipment with the aircraft to read or modify characteristics of the components of the aircraft.

Abstract: A system for controlling signals coming from or going to an aircraft simulator has a first slave circuit and a second slave circuit. The second slave circuit is used to monitor signals coming from the aircraft simulator. A multiplexer circuit is coupled to the first slave circuit. The first slave circuit sends control signals to the multiplexer circuit for controlling digital output signals being sent to the aircraft simulator. A master controller is coupled to the first slave circuit and the second slave circuit. The master controller is used for controlling operation of the first and second slave circuit. A computer system is coupled to the master controller. The computer system will display a listing of the aircraft simulator signals to be controlled. Selection of a desired aircraft simulator signal by an input device of the computer system will allow one to control the selected aircraft simulator signal.

Abstract: The present invention relates to a simulator comprising at least one projector arranged to project an image, and a non-spherical, generally continuous, dome-like projection surface on which the image is displayed.

Abstract: A flight simulator yoke is provided having a single handle having a handgrip and yoke shaft operable from a left side of a user, wherein a neutral position for the handle is at a 45 degree angle. The yoke may further include two trim axes traverse to each other; and two moveable spring devices. The spring devices are operatively coupled to the trim axes, each spring device having a positive center detent, wherein the positive center detent requires a predetermined amount of force in order to move the yoke along each trim axis. The flight simulator yoke may simulate a yoke of a Cirrus aircraft.

Abstract: An expert system and method for aircraft mission modeling using a matrix application, a preferred embodiment of which is incorporated into Mission Modeler software used in conjunction with Satellite Toolkit (STK) software. More generally, the invention is an expert system that draws on an extensive set of basic building blocks that represent standard aircraft maneuvers and concepts, and assembles those building blocks into complex and realistic sequences that represent aircraft motion with very high fidelity. One benefit of this invention is that it provides a simple system and method for users with no piloting experience to generate highly realistic flight paths.

Abstract: A smoke simulator system (1) for an aircraft simulator cockpit said system (1) comprising a water tank (2), an ultrasonic generator (3), said ultrasonic generator (3) being inside said water tank (2), supply means (7) to said water tank (2) and outlet means (8) from said water tank (2) for smoke. The invention relates as well to a method to operate such a smoke simulator system (1) for an aircraft simulator cockpit.

Abstract: A method and apparatus for managing a simulation. Information about the simulation is received over a wireless communications link with a computer system in an aircraft. The information is received during running of the simulation and identifies a performance of the computer system running the simulation. The running of the simulation is controlled based on the performance of the computer system.

Abstract: An activity device including an activity sensor generating an activity interaction signal responsive to a sustained large-muscle physical activity of a user operating the activity device; a controller, coupled to the activity monitor, generating a virtual environment supporting a virtual user frame-of-reference in the virtual environment, the controller generating a set of virtual education elements in the environment and a goal for the set virtual representation with respect to the virtual education elements wherein the controller is responsive to the activity interaction signal to produce an affected interaction of the virtual representation with the virtual education elements with the controller measuring a conformation of the goal by the affected interaction; and a feedback system, coupled to the controller, presenting the virtual environment with the frame-of-reference in relation to the virtual education elements providing the user with feedback regarding the goal and the conformation of the goal by the

Abstract: A low-cost training and synthetic visualization system and method directed to improving an individual's airborne performance in general aviation, skydiving, and other aerial applications. The system is comprised of a self-contained mobile sensor and data storage device for recording the travel path, orientation, and forces acting upon an object as it moves through space, a desktop graphics software program for creating a playback of the recorded data on a three-dimensional representation of the environment through which the object moved, a means of linking the sensor and data storage device to the software program for the purpose of exchanging information, and a centralized data storage and retrieval system designed to accept, assimilate and redistribute the recorded data.

Abstract: A method for simulating and testing avionics in a low cost PC-based flight simulator, including: converting simulator data into standard avionics messages; transmitting the avionics messages to other devices linked to the avionics simulator; receiving avionics messages and converting them to simulator data elements; and writing the simulator data elements into a flight simulators data parameters.

Abstract: A vehicle simulation system equipped to display information on the rear side of a driver (rider). The simulation system includes a dummy bicycle operated by the rider, a monitor on the front side for displaying a scene based on the operations of the dummy bicycle, and a lamp unit connected to the dummy bicycle and provided on the rear side relative to the seated position of the rider. The lamp unit has a red lamp, a yellow lamp and a green lamp, and is controlledly turned ON under the action of a main control unit. An input device is provided on a steering handle of the dummy bicycle. The input device has a switch for red, a switch for yellow, and a switch for green. The rider checks behind, and operates the input device according to the ON/OFF conditions of the lamp unit.

Abstract: An air rescue simulator, wherein the simulator comprises a helicopter passenger cabin, which is attached to a crane system.

Abstract: A radio control transmitter for a model is disclosed wherein a control range is limited to not to exceed a maximum control range without using a mechanical means. In accordance with the transmitter, an added control range being a sum of two or more of the control ranges is calculated, whether the added control range exceeds a maximum control range set to correspond to the operating section of the object to be controlled is determined, and the control range is corrected when the added control range exceeds the maximum control range.

Abstract: A method for designing a flight vehicle includes determining a preferred aerodynamic shape of a structure of the vehicle; modifying the preferred aerodynamic shape based upon constraints; and determining, using aerodynamic computational fluid dynamics, limit loading conditions for the modified aerodynamic shape. A computer-implemented system for designing a flight vehicle includes at least one computer operable to determine a preferred aerodynamic shape of a structure of the vehicle; modify the preferred aerodynamic shape based upon constraints; and determine, using aerodynamic computational fluid dynamics, limit loading conditions for the modified aerodynamic shape.

Abstract: A search and rescue training simulator and method. The training simulator comprises a first generating means, a second generating means, a third generating means, and a fourth generating means. The first generating means generates a simulated vehicle in motion performing a search and rescue function. The simulated vehicle includes a vehicular control panel. The second generating means generates a simulated environment. The third generating means generates a simulated receiver apparatus within the vehicular control panel. The fourth generating means generates a simulated transmitter apparatus within the simulated environment. The simulated transmitter apparatus is adapted to generate and transmit a signal. The simulated receiver apparatus is adapted to receive the signal and assist a user in locating the simulated transmitter apparatus in the simulated environment.

Abstract: 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.

Abstract: A low-cost training and synthetic visualization system and method directed to improving an individual's airborne performance in general aviation, skydiving, and other aerial applications. The system is comprised of a self-contained mobile sensor and data storage device for recording the travel path, orientation, and forces acting upon an object as it moves through space, a desktop graphics software program for creating a playback of the recorded data on a three-dimensional representation of the environment through which the object moved, a means of linking the sensor and data storage device to the software program for the purpose of exchanging information, and a centralized data storage and retrieval system designed to accept, assimilate and redistribute the recorded data.

Abstract: A device arranged to illuminate an area. The device includes a light source arranged to transmit a light lobe coded with information, and having a predetermined solid angle defining the width of the lobe. The light lobe is expandable/compressible between a first mode in which the light lobe has a first predetermined solid angle and a second mode in which the light lobe has a second predetermined solid angle. The light lobe is arranged to carry first information in the first mode and second information in the second mode.

Abstract: 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).

Abstract: A multi-media/simulation training system, in conjunction with a specifically developed and utilized training process, that improves target recognition skills and enhances gunnery training. The system has implications in other cognitive development activities, as well as—but not limited to—medical, technological, biological, anthropological and other areas of study with objects requiring accurate recognition and designation, as well as personnel identification devices, games, and entertainment systems. The system uses a combination of verbal and visual error correction, including magnification and rotation of both the test image and the incorrect image identified by the trainee, to enhance observation and knowledge of visible differences.

Abstract: A vehicle simulator having a projection system for projecting a generated scene and symbology onto a common viewing screen. Tracking apparatus is provided for providing position and/or angular orientation signals representative of the eye of a person viewing the projected scene and symbology. An image generation system is included for generating the scene and symbology for the projection system, such scene and symbology being generated as a function of the position and/or angular orientation signals provided by the tracking apparatus. Such symbology is representative of symbology produced by a head-up display. The image generation system generates the scene and symbology with characteristics which simulate vignetting and/or occulting effect characteristics of the head-up display.

Abstract: The invention relates to a motion and orientation simulator with a cardanic suspension (4) for a cabin (5) that is carried by a heave carriage (3) that can be moved in a straight line in a carriage cage (2), characterized in that the carriage cage (2) is rotatable and that a cable drive is provided for the straight-line movement of the carriage (3) in the carriage cage (2).

Abstract: A method is present for flight crew training. Flight crew interactions are recorded during a lesson to form recorded flight crew interactions. Flight deck displays occurring during the lesson are recorded to form recorded flight deck displays. A flight training video is formed from the recorded flight crew interactions and the recorded flight deck displays.

Abstract: A world-wide repositioning and monitoring tool for a simulated vehicle combining the features of a virtual globe or other geographic information systems (GIS) database with a navigation database allowing the operator expanded capability in terms of selecting specific or random points for relocation, eliminating the need for tedious operator input regarding points outside of the limited navigation database, and allowing a graphic monitoring tool to view and record the geographic position of the simulated vehicle.

Abstract: An adjustable video game cockpit that facilitates a number of independent adjustments to accommodate users of all sizes. The video game cockpit may include a video monitor stand and a universal video game console mount. The inclusion of the video monitor stand and universal video game console permit the cockpit to operate as a single gaming unit. The video game cockpit collapses down to a low profile for convenient relocation and storage.

Abstract: A flight motion simulator includes a pitch frame pivotably mounted, and nested for pitching in a roll frame. The roll frame is pivotally mounted to, and nested for rolling in, a base frame. The roll frame and pitch frame are rotatable in unison so as to simulate a roll of an aircraft relative to the base frame. The pitch frame is rotatable relative to the roll frame so as to simulate a pitch of the aircraft relative to the roll frame. A control stick is pivotably mounted to the base frame and pitch frame for controlling and actuating the pitch and roll. A first coupler having at least two degrees of freedom is rotatably mounted to the lower end of the control stick and to the pitch frame. A second coupler also having at least two degrees of freedom is rotatably mounted to the control stick at a lower mid-section thereof to an upper end of a post mounted to the base frame.

Abstract: Embodiments include systems and methods for assisting an operator (e.g., a pilot) of an apparatus (e.g., an aircraft) that includes a control compartment (e.g., a cockpit). The system includes a near-eye display and a processing subsystem. The near-eye display includes a transparent display panel and is adapted to be worn on a head of the operator. The processing subsystem is adapted to receive layout information defining a physical layout of one or more operational components located within the control compartment. The processing subsystem is further adapted to determine a location for a display indicator on the transparent display panel, where the location is determined to appear to the operator to be in proximity to an operational component. The processing subsystem is further adapted to generate a display signal to cause the near-eye display to display the display indicator in the location.