Abstract: In an automotive lane deviation avoidance system that prevents a host vehicle from deviating from its driving lane by correcting the host vehicle's course in a direction that avoids the host vehicle's lane deviation in the presence of a possibility of the host vehicle's lane deviation, the system calculates a desired yawing moment needed to avoid the host vehicle's lane deviation from the driving lane. The system compensates for the desired yawing moment by a correction factor or a gain, which is determined based on a throttle opening of the host vehicle.

Abstract: According to a parking assist device and a method for assisting parking of the invention, when a parking assist is canceled after a start of the parking assist, and the parking assist is restarted, a target parking position (P2B) is reset at a reset position (P1B). In the invention, at this time, the target parking position (P2B) is determined based on a target parking position (P2A) which is set at a parking preparation position (P1A), and the determined target parking position (P2B) is displayed on a screen of a monitor (4) as a default display position of a target parking frame (11) at a reset time.

Abstract: A method and apparatus for conducting proximity operations is disclosed. The method called inverser proximity operations includes maneuvering an active vehicle into general proximity to a target vehicle, transmitting from the target vehicle to the active vehicle data representing relative position and velocity between the target vehicle and the active vehicle, and maneuvering the active vehicle in accordance with the data to effect a desired proximity operation. Another method called distributed proximity operations includes maneuvering a carrier vehicle into general proximity to a target vehicle, releasing one or more active vehicles from the carrier vehicle, transmitting from the carrier vehicle to the active vehicle(s) data representing relative position and velocity between the target vehicle and the active vehicle, and maneuvering the active vehicle(s) in accordance with the data to effect a desired proximity operation.

Abstract: A military command and control system includes functional portions which respond to a set of or plurality of commands. Certain commands are mandatory. Specific responses are made in response to the mandatory commands. System tracks are handled differently than local tracks. Command and control systems which use the mandatory command structure are more readily upgraded than prior-art integrated command and control systems.

Abstract: A remote control signal, such as a signal from a GPS satellite, is received at a servant aircraft. If the remote control signal is valid, a processor on the servant aircraft prevents or inhibits anyone on the servant aircraft from controlling the flight or course of the servant aircraft. The remote control signal controls the flight and/or course of the servant aircraft. The remote control signal may come from an escort aircraft.

Abstract: The image processor of the present invention generates a more natural synthesized image from camera images taken with a plurality of cameras capturing the surroundings of a vehicle. A parameter storage section stores a plurality of image synthesis parameter groups representing the correspondence between the camera images and the synthesized image and having different spatial or temporal resolution relations. A parameter selection section selects the image synthesis parameter group according to the output of a vehicle motion detection section for detecting the motion of the vehicle such as the driving speed and direction. An image synthesis section generates the synthesized image from the camera images according to the selected image synthesis parameter group.

Abstract: Behavior-based models of robotic coordination are integrated into a synthetic hybrid control architecture of a multi-robotic system (MRS). The MRS uses rules to organize the priorities of squads of mobile robotic vehicles (MRVs) in a broader system that includes a central control model for planning, hierarchy and simulations. The system, and methods and apparatus thereof, is applied to the organization of the swarm weapon system.

Abstract: A system is described for a sensor network comprised of an apparatus of a group of mobile robotic vehicles (MRVs). The sensors in the MRVs are linked into a network such that sensor data from one MRV can be used by another MRV. The collective of MRVs can reconfigure in spatial positions and thereby responds to and interacts with its environment. The mobile sensor network is used to provide sensor data to the swarm weapon system.

Abstract: A method and system are provided for predicting and detecting the crossing of two target tracks in a bearing versus time coordinate frame. The method/system use a series of periodic bearing measurements of the two target tracks to determine a bearing rate and a projected intercept with a bearing axis of the bearing versus time coordinate frame. A crossing time tc for the two target tracks is determined using the tracks' bearing rates and projected intercepts. A prediction that the two target tracks will cross results if a first inequality is satisfied while a detection that the two target tracks have crossed results if a second inequality is satisfied.

Abstract: A collision prediction and maneuver method determines which ones of many potential target objects have a close conjunction within a gross miss distance with a subject object by trajectory propagation, then determines which one of the conjunctive objects have a high collision probability within a critical miss distance, and then determines an optimum vehicle maneuver to reduce the probability of colliding with another colliding object by determining the maneuver direction, magnitude, and time so that the least amount of propellant is consumed while avoiding potential collisions within miss distance margins. The method includes computational efficiencies in collision probability calculations using trajectory propagations and contour integrations and efficiencies in optimum avoidance maneuvering using gradient and searching computations.

Abstract: A method and apparatus for directing a pursuing vehicle, such as a torpedo, on an intercept trajectory from a launching vehicle to a target vehicle with evasion capabilities. The guidance system bases a solution on vectors on a first Cartesian coordinate system. Evasive maneuvers for the target vehicle are based upon vectors on a second Cartesian coordinate system. The guidance system converts the evasive maneuver to the first coordinate system and then performs an iterative process using initial guidance parameter values to determine, upon convergence of the solutions, final guidance parameters for the target vehicle.

Abstract: A method for estimating the curvature in a road is disclosed. The method measures an azimuth angle range and relative velocity between a host and a target vehicle, which determines whether a host vehicle is changing lanes or whether a target vehicle is changing lanes. The method calculates a heading angle of the host vehicle and calculates a corrected azimuth angle by adjusting the measured azimuth angle by the value of calculated heading angle. This method selects a curve that minimizes the mean square error between the curve and selected targets; and determines an equation that describes the curve, wherein the equation is used to predict the path head of the host vehicle.

Abstract: A navigational system for surface vessels that provides warning of impending grounding occurrences. A data base of bottom contours and submerged obstructions is compared to various indicators of the surface vessel's position and motion to provide alerts and to display bottom hazards ahead of the vessel.

Abstract: Processing GPS signals received at moving targets and at a fixed location near instrumentation associated with timing and recording an event allows the determination of instantaneous target position to be made without a requirement for additional active tracking. An example is the recording and display of a test event involving a missile intercepting a target. The missile, target, and an instrumentation site all receive GPS signals. The signals are time tagged and the data contained thereon verified by a source and forwarded from each platform to a ground station. The data is correlated with other test data to provide a real time record and display of the missile intercepting the target. Both Time Space Position Information (TSPI) and Miss Distance Indication (MDI) are derived to a very high degree of accuracy using double difference error correction techniques. Both absolute and relative position information can be derived.

Abstract: The preparation of an avoidance path in the horizontal plane so that an aircraft can resolve a conflict of routes with another aircraft that entails a risk of collision within 5 to 10 minutes. This avoidance path minimizes the negative effects of the resultant route diversion on the flight plan of the aircraft. A method prepares an avoidance path with two parts. The first part is an evasive part with an initial heading such that the threatening aircraft takes a path, in relation to the threatened aircraft, that is tangential, on one side or the other, to the edges of the angle at which the threatening aircraft perceives a circle of protection plotted around the threatened aircraft. The radius of this circle of protection is equal to a minimum permissible separation distance. The second part of the evasive path is that of homing in on the initial route. This method of preparing an avoidance path can be implemented by a flight management computer.

Abstract: A system is disclosed for computing least cost paths under hard constraints such as turn angle constraints. In an explicit embodiment, a transformation is performed on a graph representation of an optimization problem to generate a transformed graph incorporating the hard constraint in the edges of the transformed graph. Unconstrained optimization is then performed on the transformed graph using an implementation of Dijkstra's algorithm. The structure of the transformed graph lends itself to searching for an optimal solution using data structures of the vertices of the original graph. In an implicit embodiment, the searching is performed using the data structures but without explicitly generating the transformed graph. The enhanced performance of the invention is sufficient to allow for dynamic re-routing of vehicles in uncertain or changing environments.

Abstract: A drive of a primary transportation means is navigated by a navigation device along a calculated route from a starting point to a destination by the device issuing appropriate travel advice, in that a transfer location from the primary transportation means to a secondary transportation means traveling to an ultimate destination is selected for the above destination, and additional information is produced in dependence on known departure times and destinations of various ones of the secondary transportation means for use in at least one of bringing such additional information to the driver's attention and calculating the route.

Abstract: A system and method for filtering various targets (such as ground vehicles, stationary objects, and aircraft) from display on a display screen within the cockpit of an “Own Ship” aircraft. The system and method withhold from display any non-exempt targets that have an altitude that is either: (1) greater than an upper-threshold altitude; or (2) less than a lower-threshold altitude. The upper-threshold altitude and the lower-threshold altitude may be set to user-specified, customized values as desired to accommodate current flying conditions. In addition, the system and method may also be configured to operate in a plurality of operating modes, each of which features a different upper threshold altitude/lower threshold altitude combination. The system and method are preferably configured to reset certain threshold altitudes to pre-defined default altitudes in response to the aircraft landing.

Abstract: A vehicle environment monitoring system for an automotive vehicle is capable of accurately detecting the movement of an object existing in an environment of the vehicle, and determining the possibility of collision between the object and the vehicle, thereby appropriately warning the driver. A relative position of the object to the automotive vehicle is detected from the image obtained by a camera mounted on the vehicle to obtain position data. Positions of the object in a real space are calculated based on a plurality of time series items of the position data detected on the object, and a movement vector of the object is calculated based on the positions in the real space. It is determined based on the movement vector whether or not the object has a high possibility of collision against the automotive vehicle.

Abstract: Paths are planned for one or more actors, through at least two dimensions of time or space, to identify rendezvous locations meeting a global criterion. At least two scenarios are defined, including at least one for each actor, and a configuration space is created for each of these scenarios. A scenario includes identification of the actor, a source direction for planning, a set of states identifying the source or obstacle locations, and the respective cost metrics for each possible transition between a configuration state in the corresponding configuration space, and its neighbors. Cost waves are propagated in each configuration space, to generate a cost-to-source for each state. A Boolean evaluation is then made of configuration states, according to a global criterion, to identify all possible rendezvous states. Finally, the actors are controlled to travel to that rendezvous chosen according to optimization criteria, or the candidate rendezvous states are displayed for further evaluation or use.

Abstract: A lateral deviation &dgr;d which is a lateral distance between an intrinsic appropriate course R for a vehicle Ai and a contact position P at which the vehicle Ai will come into contact with an on-coming vehicle Ao, is calculated based on a relative angle &thgr;, a relative distance L and a relative speed Vs which are detected by a radar device, and based on a vehicle speed Vi of the vehicle Ai detected by vehicle speed sensors. When the lateral deviation &dgr;d is in a range of &dgr;dn<&dgr;d<&dgr;dx, it is determined that there is the possibility that the vehicle Ai will collide frontally with the on-coming vehicle Ao. The lateral deviation &dgr;d can be calculated based on the relative angle &thgr;, the relative distance L and the relative speed Vs provided in one cycle of transmission and reception of beam by the radar device.

Abstract: A method for the automated generation of ballistic constants for use in a trajectory control system. The potential trajectory of a pursuing vehicle is divided into a plurality of multiple sequential phases wherein each phase is characterized by a plurality of ballistic parameters. Known simulated data from a number of runs concerning the pursuing vehicle is analyzed. Ballistic parameter values for each run are obtained and statistically analyzed to produce generic constants for a particular set of operating conditions. Resulting matrices are stored as part of a two-dimensional, kinematic vehicle model to facilitate the propagation of projected trajectories during firing control solutions.

Abstract: An apparatus for improving the reliability of a course generator of a moving body and the efficiency of the moving body. When the tangent (53) of a scheduled course (50) at its branch point (PS) is in parallel with a line segment (54) coincident with the traveling direction of the moving body (20) at the end point (PL) of a branch course (52), the branch course (52) is generated from a cubic curve having one extreme coincident with the branch point (PS), and the tangent of the cubic curve at this extreme coincides with the tangent (53) of the scheduled course (50) at the branch point (PS). The other extreme of the cubic curve coincides with the end point (PL) of the branch course (52), and the tangent of the curve at this extreme coincides with a line segment (54) which in turn coincides with an end point traveling direction of the moving body. A ground monitor station (40) guides and travels the moving body (20) along a modification of the branch course.

Abstract: In a method of detecting a collision risk and preventing air collisions, it is proposed that probabilities should be calculated for the likely presence of one's own aircraft in predetermined sectors at a number of selected times (probabilities of presence) and these probabilities for one's own aircraft and those for other objects should be used to calculate the probabilities of one's own aircraft and at least one of the other objects being present simultaneously in a given sector (probabilities of collision) for the predetermined sectors and selected times.

Abstract: A method of automatically controlling an aircraft to avoid a vertical zone includes several steps. The aircraft first acquires limits of the zone to be avoided. The zone is modeled by a cylindrical volume which is limited by a horizontal contour with upper and lower altitudes of the zone. The cylindrical volume associated with a scheduled route of the aircraft is located and points of entry and exit in the cylindrical volume are determined. A new flight altitude is calculated in order to avoid the zone. A point of change of altitude is calculated to reach an avoidance altitude. The new flight altitude is updated and the point of change of altitude is input into an automatic pilot.

Abstract: A method for determining an alternate path by a mobile machine to avoid at least one obstacle. The method includes the steps of assigning an initial value of charge to the mobile machine, assigning a value of charge to a desired destination, determining the presence and the locations of at least one obstacle, and assigning a value of charge to each determined obstacle. The method further includes the steps of determining a force vector equation for each of the desired destination and each obstacle with respect to the mobile machine, determining a resultant force vector as a function of the force vector equations, and controlling the steering and movement of the mobile machine in response to the resultant force vector.

Abstract: An aircraft autopilot system provides a wind correction angle which is added to the desired course to provide commanded heading, the wind correction angle being generated as a proportional and integral function of ground track error. When the aircraft is off its desired course, it can be returned to the desired course by means of a course intercept angle, added to the desired course, to provide a corrected commanded course, the course intercept angle being a proportional function of the perpendicular error (the lateral distance of the aircraft from the original course) suitably limited to some angle within 90.degree. of the desired course. The course correction angle may be generated as a proportion of the perpendicular course error determined by the degree of importance of accuracy, and may be switched over to a course directly toward a waypoint in dependence upon the importance of efficiency.

Abstract: The present automated vehicle travel path determination system which computes a travel path for a vehicle from an origination point to a destination point based on the operating characteristics of the vehicle as well as phenomena extant in the multidimensional space, which phenomena have an impact on the cost of operation of the vehicle. This vehicle travel path determination system can concurrently consider a plurality of vehicle operating characteristics in selecting the travel path. The travel path is optimized for a weighted selection of a number of cost factors, which weighted selection represents a desired combination of cost factors for the operation of this particular vehicle. This vehicle travel path determination system also considers the time varying nature of the phenomena that exist within the multidimensional space and the impact these time varying phenomena have on the vehicle as it traverses the travel path.

Abstract: A driving force control apparatus for moving a vehicle by a desired distance includes an input section for input a desired move distance, a throttle controller section for setting a throttle actuator of the vehicle at an opening degree, an actual moved distance detecting section for detecting an actual moved distance of the vehicle, and a braking section for stopping the vehicle by braking when the vehicle moved the desired distance. Therefore, a slight movement of the vehicle is simplified and therefore the load to a vehicle driver is decreased.

Abstract: A method and apparatus for directing a pursuing vehicle, such as a torpedo, on an intercept trajectory from a launching vehicle to a target vehicle th evasion capabilities. Models of the pursuing vehicle and evading target provide proposed trajectories based upon various environmental considerations. A guidance system uses estimates of initial operating parameter solutions, such as gyro angle, alertment time and intercept time, to begin a convergent, iterative process that defines final operating parameter solutions from which the guidance parameters are determined and transferred to the pursuing vehicle at launch. During each iteration, the solution determines an alertment time and an alertment bearing from the target vehicle to the pursuing vehicle at the alertment time. A selected evasive strategy includes a turn that is calculated relative to the alertment bearing.

Abstract: A virtual image display system for aircraft is operative to identify threat systems that are proximal the flight path of an aircraft when the aircraft is within the threat range of such threat systems. The virtual image display system is further operative to generate three-dimensional threat envelopes of identified threat systems and to display real-time perspective video images of such three-dimensional threat envelopes for viewing by the pilot.

Abstract: The present invention is a fire control system. The fire control system comprises a manually aimed gun having a sighting device and a device for acquiring a target. The acquiring device is disposed at a location remote from the gun. The fire control system also comprises a device for determining the trajectory of the target with respect to the gun and providing information relating to the target to the sighting device of the gun such that an operator of the gun can aim the gun with respect to the sighting device to hit the target when the gun is fired. The determining device is in communication with the acquiring device and the sighting device. The present invention is also a fire control method for a minor caliber gun. The method comprises the step of acquiring a target from a location which is remote from the gun. Then, there is the step of determining the trajectory of the target with respect to the gun.

Abstract: Two new adaptive homing guidance laws are developed which are variants of Augmented Proportional Navigation (PRONAV). The first guidance law commands flight path angle rate and is referred to as adaptive matched augmented PRONAV (AMAAP). The second guidance law commands linear acceleration and is referred to as adaptive matched augmented linear PRONAV (AMALP). The major attributes of these guidance laws are (1) they are the solutions of a linear quadratic control problem, (2) they do not require an estimate of time-to-go (tgo), (3) they are matched to a nonlinear model of the target's motion, (4) they adapt in real time to provide optimal guidance over each small segment of the intercept trajectory, and (5) they optimally account for missile deceleration.