Abstract: A control system includes a ride controller configured to maintain a plurality of rules indicative of permitted states of the free-roaming ride vehicle within a game area and including gameplay rules. The ride controller is configured to receive monitoring data indicative of a current state of a free-roaming ride vehicle, receive a signal indicative of a user request to perform a requested action with the free-roaming ride vehicle, model performance of the requested action from the current state to determine a modeled state of the free-roaming ride vehicle, and determine whether the modeled state complies with the plurality of rules. In response to determining the modeled state does not comply with the plurality of rules, the ride controller is configured to determine a proximate action that complies with the plurality of rules and provide a control signal to instruct the free-roaming ride vehicle to perform the proximate action.

Abstract: A motion and vibration cuing system for use with a motion simulator provides vibratory, impulse, onset and sustained motion cuing, independently or simultaneously, by operation of a frame assembly capable of producing vibration and six degrees-of-freedom of motion in coordination with one or more motion seats, mounted to the frame assembly, which produce surge, sway, heave and roll motions.

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: 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: The invention relates to a flight simulator vibration system, particularly to a crew seat (1), a flight control stick (20) and a panel (30) vibration system of a flight simulator with at least one plate of the crew seat (1), the flight control stick (20) and/or the panel (30) being equipped with predefined momentum weights (13, 16) and electric motors driving said respective momentum weights. Speed governors are controlling individually said electric motors (7, 8, 9, 21, 33, 34).

Abstract: A multiple degree-of-freedom motion simulator assembly comprises a fixed base, a displaceable simulator platform, and a plurality of linear actuators having upper ends thereof interconnected with the platform and lower ends thereof interconnected with the fixed base. A vibration damping unit is disposed between at least one of each of the upper ends and the platform and each of the lower ends and the fixed base. The damping units include at least a first resilient member preloaded and mounted to a major surface of a plate of the damping unit engaged to one of the ends of the linear actuator. The first resilient member provides vibration absorption such as to damp vibrations transmitted from the plate to the platform or base in at least a direction substantially perpendicular to the major surface.

Abstract: Interactive simulation including force feedback. The system includes a computer game display unit programmed with simulation rules. A control unit is connected to the computer and provides information and control signals to the computer to interact with the stored simulation rules and to receive information and control signals from the computer. A movable structure for movement in at least two degrees-of-freedom by an operator is interconnected to the control unit by actuators. A programmable unit processes signals and information from the computer to generate signals to drive the actuators so as to apply forces in the at least two degrees-of-freedom to the movable structure and thereby to the operator. The applied forces are based on internal programming within the programmable unit, events occurring in the simulation and movements of and forces applied to the movable structure by the operator.

Abstract: A method and an apparatus for determining at least one property of a multiphase fluid. The method includes the steps of directing the multiphase fluid through a first flow passage, monitoring the multiphase fluid as it passes through the first flow passage to obtain a first signal representing a first flow characteristic of the multiphase fluid as a function of time, directing the multiphase fluid through a second flow passage, monitoring the multiphase fluid as it passes through the second flow passage to obtain a second signal representing a second flow characteristic of the multiphase fluid as a function of time, and then determining the property of the multiphase fluid by comparing the first signal and the second signal with a set of calibration maps. The second flow passage has a geometry different from the first flow passage which relates either to the cross section of the two flow passages or to the direction in which the multiphase fluid passes through the flow passages relative to gravity.

Abstract: A flight simulator includes a central processing unit and a flight simulation environment controlled by the central processing unit for simulating the flight of an aircraft. The central processing unit is programmed to observe a full fidelity model of the aircraft in flight so as to extract pilot inputs and aircraft responses at each of successive time intervals. The central processing unit is further programmed to calculate a damping and an undamped natural frequency of the aircraft from the extracted pilot inputs and aircraft responses and to simulate the flight of the aircraft by applying the damping and undamped natural frequency to a second order transfer function.

Abstract: A virtual reality system provides effective exposure treatment for psychiatric patients suffering from a particular anxiety disorder. The system is characterized by a video screen disposed in front of the patient to display an image of a specific graphical environment that is intended to trigger anxiety within the patient as a result of the particular patient phobia. A headset is worn by the patient, and has sensors disposed to detect movement and positioning of the patient's head. A computer program controls the operation of the system, and is designed to control the display of the graphical environment on the video screen, monitor the headset sensors and determine the position of the patient's head, and controllably manipulate the graphical environment displayed on the video screen to reflect the movement and position of the patient's head.

Abstract: A transportable three-dimensional calibration wind tunnel system is comprised of a small wind tunnel portion for creating a three-dimensional calibration air having a suitable wind velocity, and a two-axis rotational deformation device portion for causing said wind tunnel portion to effect a conical motion with a nozzle blow port being an apex to suitably change a flow angle. The two-axis rotational deformation device is comprised of a .beta.-angle rotational deformation device having a .beta.-angle deformation base supported to be rotated horizontally, and a .alpha.-angle rotational deformation device having a .alpha.-angle deformation base supported to be rotated vertically. A rotational axis of the .alpha.-angle deformation base, a rotational axis of the .beta.-angle deformation base and a center axis of the small wind tunnel portion are arranged so that they intersect at a point.

Abstract: A method of manufacturing a motion simulator having a deck and a number of deck-supporting legs (2) that are pivotally connected with the deck in first pivot points (4). The legs are actively and continuously length-adjustable, such that the deck is capable of describing a motion envelope comprising all desired deck positions, wherein a leg envelope is determined for each leg within which the possible positions of the relevant leg are located, whereafter the common surrounding space of the legs, and in particular the interspace included between the leg envelopes is determined. A shell is then designed that at least carries the deck, which shell defines an inner space extending at least partly within the interspace between the legs (2) defined by the leg envelopes, in such a manner that in each position of the simulator, the legs are clear of the shell (1).

Abstract: Apparatus for simulating the motion of a vehicle includes a base frame, a subframe which is movable in relation to the base frame, the movements of the subframe simulating the real life movements of the vehicle, and first, second, third and fourth linkage members each connected through a universal joint both to the base frame as well as to the subframe. The first and second linkage members are positioned in a first imaginary plane and the third and fourth linkage members are positioned in a second imaginary plane, the first and second imaginary plane intersecting each other at a first intersection line. The first and third linkage members are positioned in a third imaginary plane and the second and fourth linkage members are positioned in a fourth imaginary plane, the second and fourth imaginary plane intersecting each other at a second intersection line. The first and second intersection lines cross each other at right angles.

Abstract: A virtual reality system provides effective exposure treatment for psychiatric patients suffering from a particular anxiety disorder. The system is characterized by a video screen disposed in front of the patient to display an image of a specific graphical environment that is intended to trigger anxiety within the patient as a result of the particular patient phobia. A headset is worn by the patient, and has sensors disposed to detect movement and positioning of the patient's head. A computer program controls the operation of the system, and is designed to control the display of the graphical environment on the video screen, monitor the headset sensors and determine the position of the patient's head, and controllably manipulate the graphical environment displayed on the video screen to reflect the movement and position of the patient's head.

Abstract: Spatial disorientation trainer-flight simulator wherein a cockpit is gimballed on three independently-controlled axes, i.e., pitch, roll and yaw, which revolve about a planetary axis. Rotation of the cockpit about the planetary axis is controlled by a remote console computer. Rotation of the cockpit about the pitch and roll axes is controlled by an on board cockpit computer alone or in combination with the console computer. Rotation of the cockpit about the yaw axis is controlled by the console computer alone or in combination with the cockpit computer. Slip rings are employed at the planetary and yaw axes so as to provide 360.degree. cockpit rotation about each axis. Rotation about each of the pitch, roll and yaw axes is effected by a high torque direct drive dc motor under control of the computers. Smooth, continuous motor operation is possible over a wide range of speeds, including sub-threshold speeds not detectable by the pilot.

Abstract: Method and apparatus for driving the motion system of a flight trainer to simulate aircraft buffeting which method and apparatus avoids the resonant frequency of the motion systems hydraulic actuators by using a "Linear Tracking Band-Stop Filter". Band-stop filter circuitry is combined with linear tracking band pass filter circuitry to provide the linear tracking band-stop filter. This circuit receives command signals intended for the servoamplifier used to drive a hydraulic actuator. The band-stop filter eliminates or substantially attenuates those frequencies contained in the command signal which would cause resonance of the hydraulic actuator. It has been discovered that the resonance frequency of the hydraulic actuator varies as a function of the extension of the actuator, and therefore in this invention the center frequency of the band-stop filter tracks the resonant frequency of the actuator such that a much smaller band of frequencies is eliminated.