Abstract: A rotor setting system in conjunction with an aerodynamic-body control. The setting system is characterized by a rotor which comprises a console, a rotary drive for the rotor, setting members for the control of the aerodynamic body, especially rudders or spoilers, as well as a control unit for the rotor, and further including a control unit on the sides of the aerodynamic body, wherein the two control units cooperate with each other for adjusting the setting members.

Abstract: A measuring device for the location and attitude determination of an object, for example, of a space craft for the purpose of docking. At the object several light sources are located, each intensity-modulated with a different code frequency. Optics of the measuring device reproduce the object on a position-sensitive detector. On the basis of its output signals, the image coordinates of the light sources are computed by way of an evaluating device using a frequency multiplexing process.

Abstract: An undercarriage with a wheel set capable of self-steering independent of the vehicle body is disclosed. The undercarriage contains, in combination with hollow profile wheels in the wheel sets and primary elastic springs in the longitudinal direction, two lever systems which are self-adjusting, independent of each other and are arranged on the longitudinal sides of an undercarriage. The lever systems forcibly couple the axle ends of the wheel sets on the same rail in the longitudinal direction of the undercarriage and are movable only in opposite directions.

Abstract: A strapdown measuring unit for measuring the angular velocities about the three axes of a flying body rotating relatively fast about its first axis is disclosed. The unit combines a Sagnac effect sensor for roll rate determination and two micro-mechanical acceleration sensors whose output, combined mathematically with the output of the Sagnac effect sensor, determines the angular velocity of the remaining two axes. The mathematical calculations are performed by a dedicated microprocessor which is integrated with the three sensors into a single small unit.

Abstract: A device for allowing the adjustment of the length of a fiber optic waveguide is disclosed. The device couples casings of different inner and outer diameters together, while allowing for the movement of the fiber optic waveguide within the casings. The device is useful for adapting the fiber optic guide to different instruments, such as endoscopes.

Abstract: A hollow insert for a sandwich structure having at least one fixed head on a substantially hollow cylindrical shank with a bore through the shank, the head being eccentric relative to the shank, with a corresponding eccentricity of the opening of the bore of the shank in the head, the eccentricity securing the insert against rotation in the structure.

Abstract: An improved shaft for a munition firing apparatus is disclosed. The shaft has a multiplicity of approximately curved firing channels and is supported in the firing apparatus in a low friction manner.

Abstract: A missile with adjustable flight controls capable of altering the missile's flight path is disclosed. The missile comprises an electric generator and control electronics. The electric generator is used in this invention both to provide electrical power to the control electronics and to regulate the flight controls. A mechanical connection is created between the generators rotor and the flight controls. The generator is electrically coupled to the control electronics through an electrically variable load. The control electronics alters the load which varies the rotational speed of the generator. This in turn affects the flight controls and the flight path is altered accordingly. The invention is small and compact, allowing its use in small missiles such as mortar or artillery shells.

Abstract: A frequency-selective sound transducer comprised of a number of resonators with differing but sequential natural frequencies arranged in a first plane. A deformable membrane is arranged in a second plane, parallel to the first plane and in close proximity thereto. A small air gap thus exists between the first and second planes. Sound waves produce vibratory motion in the membrane, which motion is transmitted to the resonators by pressure waves generated by the membrane in the air between the membrane and resonators. The deflections of the resonators are converted into electrical signals.

Abstract: A radiation coagulator with a radiation source which has a large infrared content and with a sleeve-shaped cap which is placed on the holding tube at the radiation exit end of the light conductor, and with which the area of the tissue to be coagulated is brought into contact.

Abstract: This method serves for calibrating gyros forming part of the attitude control system of a satellite stabilized in three axes and which have an unknown drift. A two-axis sensor measuring the direction of a radiating reference object in the coordinate system x, y, z fixed with respect to the satellite is used. Two reference attitudes each different with respect to the reference object are commanded to the satellite in the course of two consecutive time intervals spaced from each other. The values measured by the sensor representing the respective actual direction of the reference object are recorded at the start and at the end of the time intervals. The respective time integrals of the gyro output signals are computed during the time intervals, which represent the gyro drift plus the respective instantaneous satellite deviation from the commanded reference attitude. Finally the gyro drift is determined from these time integrals and the values measured by the sensor.

Abstract: For the circumferential irradiation of objects, especially of vessels, hollow organs and solid tissue, by optical radiation of high intensity which is conducted via a flexible optical fiber, the optical radiation is coupled into the optical fiber at a predetermined angle (.beta..sub.1,.beta..sub.2) to the surface normal of the end face of the optical fiber such that it leaves the distant end of the optical fiber in the form of a conical surface.

Abstract: An optical system for motion compensation of line scanners to improve the resolution in one or more spectral channels, the system having a motion of its own or being arranged on a moving observation platform. A multi-faced prism is provided which is associated with the optical system and rotates about its central axis at a settable rotational speed. The integration time for imaging a radiation source is increased due to the rotation of the prism in a direction opposite the track or flight direction.

Abstract: A device for adjusting the polarization plane in an antenna feed system is disclosed. The rotary device uses flexible waveguides which permits rotation of the polarization plane over a large angular range.

Abstract: A method for controlling a magnet of a magnetically levitated railroad, wherein at least three variables are used which are acquired in an observer unit (support circuit) based on the measured magnitudes for the magnetic gap width s, as well as the magnetic acceleration b; to improve the following behavior of the magnetically levitated vehicle without increasing the background noise component, an additional rail signal is feed to the controller of the individual magnets, which rail signal is respectively obtained by a rail observer unit from the measured magnitudes of the magnet gap width and the magnet acceleration of one of the magnets which is leading in a travel direction in such a way that it represents a noiseless rail signal with a correct phase in the useful frequency range as referred to the respectively trailing magnets.

Abstract: A disc wheel, particularly for rail vehicles, with a composite metal/plastic structure. In order to make possible simple manufacture with at the same time adequate force transmission, a structure between the hub and the tread comprises a plastic structure comprising two half shells of the same design which are subdivided in sector fashion by spoke-like reinforcement ribs. The reinforcement ribs each have a longitudinal slot into which rib plates are inserted which connect the two half shells to each other. Advantageously, plastic foam is inserted into the cavities of the half shells. All joints between the plastic structure and the hub or the tread are cemented joints.

Abstract: A reacquisition process is used in the event that an earth orientation of the yaw axis Z of an earth satellite is lost, in that the angular velocity .omega. of a flywheel, the rotational axis of which is oriented in the direction of a pitch axis Y, falls below a predetermined value as a result of an insufficient energy supply. After restoration of the energy supply, the pitch attitude of the earth satellite and, accordingly, the earth orientation of the yaw axis Z, are to be restored. For this purpose, constantly alternating increases and decreases in speed are commanded for the flywheel in a determined manner in correlation with the zero passages of the pitch deviation, whereby the satellite is subjected to a constant reversal of its direction of rotation. This occurs until the angular momentum of the satellite falls below a predetermined value during a zero passage of the pitch deviation.

Abstract: The invention relates to an apparatus for controlling a projectile (1) having a nozzle arrangement (2) rotatably arranged in the projectile housing. The nozzle arrangement comprises a rotary nozzle body (3) with a thrust nozzle (4) which nozzle body can be brought into any desired angular position by means of a positioning drive. The rotary nozzle body (3) is coupled to a gas generator (7) for a propellant gas supply. For optimum utilization of the propellant gas of the gas generator, in all angular positions of the rotary nozzle body (3), the axis of rotation (a) of the rotary nozzle body (3) is arranged to be non-parallel to the longitudinal axis (A) of the projectile.

Abstract: A fiber optic sensor for the detection of mechanical quantities comprising a light source, a first fiber optic waveguide coupled to the light source, the front face of the first waveguide being ground at a 45.degree. angle to the axis of the fiber and mirrored, a second fiber optic waveguide arranged parallel to the first waveguide, the front face of the second waveguide being ground at a 45.degree. angle to the axis of the fiber and mirrored, the two mirrored faces being held opposite to one another, and a photoelement receiver coupled to the other end of the second waveguide. At least one of the waveguides can move either along the fiber axis or around the fiber axis relative to the other waveguide, the motion varying the light received by the receiver and thereby indicating the magnitude of the mechanical quantity.

Abstract: The disclosure is directed to a modulation device for a radiation detector device picking up an image field. The modulation device comprises a modulation disk disposed in the image field plane and having radial slits, said modulation disk executing a nutation about the axis of the image field. The modulation device further includes an optical system, a radiation-sensitive receiver arrangement and a signal processor. The radiation-sensitive receiver arrangement (11) comprises a grouping of radiation reception elements (E11 to Emm) forming a radiation receiver field (13), which elements are coupled with a window circuit (18, 22, 32) and are selectively addressable by the window circuit for the formation of at least one window zone within the radiation receiver field (13). The addressing occurs such that only signals of this at least one window zone are transmitted into the signal processor.