Abstract: The invention consists of means which computes the numerical solution of an interconnected system of first order differential equations in a single computational pass. The method in effect treats the digital computer as a close approximation to an analog computer whose solutions are instantaneous. This is in contradistinction to the prior art regarding digital computer solutions of first order differential equations that utilize repetitive computational passes over the same time interval to obtain numerical solutions, and which further generates estimates of future values extrapolated from past values of state variables. The invention inserts an auxiliary function existing between, and at, the times marking the computational intervals. The invention rests on three postulates regarding the auxiliary function: a first postulate expands on the Euler formulation of the solution of a differential equation by including the unknown sought after state variable in an expanded Euler formulation.

Abstract: A paper lifter with multiple lever arms and a loose-leaf ring binder combine to form a class two lever system. A row of apertures forms a pivot axis aligned with the rings of the binder. The lifter is slidably and pivotably connected to the binder through the apertures. The connection forms a first set of contact points between the lifter and the binder. An inside edge forms a second set of contact points with the rings. The two sets constitute a first lever system. A set of load arms reaches inward from the axis of the apertures to form a third set of slidable contact points with a protective plate of the binder ring mechanism. This third set and the first set combine to form a second lever system. Curvature of the load arm provides a variable length lever arm as a function of lifter angle with the protective plate. The lifter may comprise different segments; load arms and apertures may be on different segments of the lifter.

Abstract: A system and method for cleansing a polluted harbor by achieving general circulation of water between an open sea and the polluted harbor are disclosed. The system and method utilize the natural wave-like behavior of the water when ocean tides propagate from a harbor entrance in the open sea to a back harbor and back out to sea again. Surface elevation variations along the propagating wave provide hydrostatic pressure differentials between areas along the path of propagation. When connecting two such areas with a conduit, the pressure differential between two areas causes water to flow in the conduit. The system includes a conduit which connects an area of the open sea with a back harbor area. The conduit may be installed along a channel of the harbor so that it extends through the harbor to the back bay, or it may be positioned to cut across or through a strip of land separating the back harbor from the open sea.

Abstract: A dual drive control system applicable to precision machine tools and robotics eliminates the consequences resulting from coulomb friction and stiction by avoiding the operating points where these defects manifest themselves. A first embodiment consists of a dovetail slide having a base and a motive slide, two motors, a feedscrew, and a helical gear assembly. The feedscrew is mounted parallel to the linear motive direction of the slide; a helical gear is mounted with its axis normal to the feedscrew and with its teeth meshing with the screw threads of the feedscrew. The first motor is mounted on the base and imparts rotation to the feedscrew. The second motor is mounted on the slide and imparts rotation to the helical gear. In operation, the first motor turns the feedscrew at a continuous speed. The second motor drives the helical gear so that its teeth follow the threads of the rotating feedscrew.

Abstract: A paper lifter and a loose-leaf ring binder combine to form a class two lever system. The lifter has two sets of apertures. A first set fits slidably over the rings. A curved load arm reaches inward from the apertures and abuts a plate protecting the binder ring mechanism; the curvature provides a variable length load arm with lifter angle. The contact point between the load arm and the plate becomes a system fulcrum; yet the contact point (and the lifter) is free to slide along the plate. An effort arm extends oppositely to reach and slide against the binder cover. A second set of apertures are slots in the curved load arm. The slots, in line with the rings, prevent ring interference with continuous contact between the load arm and the plate. The system fulcrum then remains on the plate for the first and critical phase of the closing motion.

Abstract: A concept for a support stand adapts an Asian WOK to a Western kitchen range. The stand provides an upper ring to receive a round bottomed WOK; the ring has sufficient diameter to accommodate the WOK securely in the stand. The base of the stand adapts to prior art drip pans placed in heating wells, where the well has gas or electrical heating elements located according to the type of range, and thus anchors the stand to the kitchen range top.A second concept modifies existing drip pans to provide both the functions of drip pan and support stand in a single, combined support stand. This stand replaces existing stands and drip pans and anchors the WOK to the kitchen range top.A third concept converts a prior WOK fire ring into a trivet allowing use of the WOK at a dinner table.

Abstract: A system and method for cleansing a harbor are disclosed which utilize the natural wave-like surface behavior of a tide wave propagating up a natural harbor or bay. Surface elevation changes along the propagating wave provide hydrostatic pressure differentials which drive the system. The system includes a conduit which connects an open sea area with an inner harbor area. The conduit may be either positioned on the bottom of harbor so that it extends through the harbor bay or it may be positioned so that it cuts across or cuts through a strip of land separating the harbor from the open sea. The conduit inlet is positioned in the open sea area and the conduit outlet is positioned in the inner harbor area. The outlet has a one way valve which both allows water flow through the conduit from the open sea area directly into the inner harbor area and also prevents water flow in the conduit in the reverse direction.

Abstract: A dual drive motive system used to control the movement or position of another system or structure in a first and second embodiment has two motors, two frame members and a ring moveably mounted between the frame members by means of suitable bearings. One of the motors provides continuous relative motion between the ring and one of the frame members which may be secured to a foundational structure. The other motor provides relative motion between the ring and the other frame member which may be secured to a turret structure. This motion avoids the transient disturbances of lubricants. In a third embodiment, the system includes two armatures which share a common stator. In operation, the armatures and stator which are concentrically positioned rotate relative to each other and in opposite directions. In a fourth embodiment, the armatures share a common stator and the armatures are coaxially positioned.

Abstract: A rate gyro instrument primarily for use in a gun fired spinning projectile eliminates all associated bearings by affixing the rotor to the spinning projectile body to obviate spin rotor bearings and by employing a flexible joint or constriction as a gimbal substitute to eliminate gimbal bearings.

Abstract: An open-loop system for controlling a plant, including a sampling circuit for providing an actuating signal as a series of impulse signals, and a computer for providing a control signal to operate the plant in response to the actuating signal in accordance with a control function defined by a control algorithm based upon a calculated response of the plant in an equivalent closed-loop linear control system. The computer provides the control signal as a function of time following the application of each impulse signal. The control algorithm is a time-domain algorithm based upon an inverse LaPlace transform of the equivalent system. The interval between impulse signals, as defined by the sampling rate, is on the order of the time constant of the equivalent system; and the computation speed of the computer is sufficiently fast to provide a control signal that is effectively continuous relative to the operating dynamics of the plant.

Abstract: A missile is disclosed which utilizes elastic deformation of structural members in order to control missile flight. The elastic deformation may be in the mounting of the rocket nozzle, the provision of deformable control surfaces, or provision of deformable sections of rocket body, all of which are controlled by independent actuating means.

Abstract: A projectile trajectory correction system, the projectile itself including a unique steering arrangement. The projectile, initially part of a shell cartridge, is fired, and its position is automatically sensed. A corrected trajectory necessary to hit a target is calculated and data commands are transmitted to the projectile. The data command signals are sensed by an antenna on the projectile. The antenna in turn generates a signal which is fed to the projectile steering mechanism which is deflected in response thereto to steer the projectile onto the correct trajectory. The steering mechanism includes an elongated rod extending from the rear of the projectile into the surrounding air stream. Deflection of the rod provides the actual steering.

Abstract: A projectile trajectory correction system, the projectile itself including a unique steering arrangement. The projectile, initially part of a shell cartridge, is fired, and its position is automatically sensed. A corrected trajectory necessary to hit a target is calculated and data commands are transmitted to the projectile. The data command signals are sensed by an antenna on the projectile. The antenna in turn generates a signal which is fed to the projectile steering mechanism which is deflected in response thereto to steer the projectile onto the correct trajectory. The steering mechanism includes an elongated rod extending from the rear of the projectile into the surrounding air stream. Deflection of the rod provides the actual steering.

Abstract: A fragile, movable apparatus such as a rotatable infrared optical prism assembly is mounted in a projectile housing on a crushable support pad. When the projectile is launched, the fragile, movable apparatus crushes the pad and receives effective support from the pad. After launch, a resilient member positions the fragile, movable apparatus away from the crushed pad and provides the necessary freedom of movement for the fragile, movable apparatus.

Abstract: A delivery system for multiple sub-missiles including in the sub-missiles a marking system, a detection system, a diverter for elimination of targets identified by the detector system, a scanner for initial determination of multiple targets, a logic circuit utilizing input from both the diverter and the scanner to eliminate targets and a sub-missile guidance system.

Abstract: A delivery system for multiple sub-missiles including in the sub-missiles a marking system, a detection system, a diverter for elimination of targets identified by the detector system, a scanner for initial determination of multiple targets, a logic circuit utilizing input from both the diverter and the scanner to eliminate targets and a sub-missile guidance system.

Abstract: A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.

Abstract: In a closed loop servo system in which the input signal is inaccessible and not available for measurement, but the error signal and output signal are both accessible and measurable, a filter configuration is provided which can be inserted into the error signal path of the system to reduce the undesirable effects of noise or other unwanted signals without appreciably affecting the closed loop dynamics of the overall system. In the generalized system a filter having the characteristics g(s) in LaPlace notation is inserted into the error signal path of the system to filter selected components of the error signal. A second filter having the characteristics h(s) which satisfies the equation g(s)+h(s)=1, is coupled between the output signal and the output of the filter having the characteristics g(s).

Abstract: An inertial guidance system including a true space stable platform is provided while retaining a simple two-degree-of-freedom gimbal system. An added third degree of freedom is provided by motions of the support itself which maintains desired platform orientation. The output of a third axis instrument is used to maneuver the frame itself about the axis of the frame which most nearly will null any rotation about the platform roll or longitudinal axis. A rotational rate gyroscope is positioned on the space stable platform, and actuates the movement of the frame about the longitudinal or roll axis directly from the reading of the rotational movement along the roll axis of the platform.

Abstract: A missile is disclosed on which constant burning thrust reaction motors are provided integral with the tail panels of the missile to enhance the effect thereof, particularly during the boost phase of flight. The motors provide thrust along the chord of the tail panel and are moved about the axis of rotation of the tail panel by the servo motor associated therewith. The servo motors are activated by central missile control circuitry.