Optical Light Curve Observations to Determine Attitude States of Space Debris

The currently proposed space debris remediation measures include the active removal of large objects and “just in time” collision avoidance by deviating the objects using, e.g., ground-based lasers. Both techniques require precise knowledge of the attitude state and state changes of the target objects. In the former case, to devise methods to grapple the target by a tug spacecraft, in the latter, to precisely propagate the orbits of potential collision partners as disturbing forces like air drag and solar radiation pressure depend on the attitude of the objects. Non-resolving optical observations of the magnitude variations, so-called light curves, are a promising technique to determine rotation or tumbling rates and the orientations of the actual rotation axis of objects, as well as their temporal changes. The 1-meter telescope ZIMLAT of the Astronomical Institute of the University of Bern has been used to collect light curves of MEO and GEO objects for a considerable period of time. Recently, light curves of Low Earth Orbit (LEO) targets were acquired as well. We present different observation methods, including active tracking using a CCD subframe readout technique, and the use of a high-speed scientific CMOS camera. Technical challenges when tracking objects with poor orbit redictions, as well as different data reduction methods are addressed. Results from a survey of abandoned rocket upper stages in LEO, examples of abandoned payloads and observations of high area-to-mass ratio debris will be resented. Eventually, first results of the analysis of these light curves are provided.

Inclination-dependent changes of the critical shoulder angle significantly influence superior glenohumeral joint stability.

BACKGROUND The critical shoulder angle combines the acromion index and glenoid inclination and has potential to discriminate between shoulders at risk for rotator cuff tear or osteoarthritis and those that are asymptomatic. However, its biomechanics, and particularly the role of the glenoid inclination, are not yet fully understood. METHODS A shoulder simulator was used to analyze the independent influence of glenoid inclination during abduction from 0 to 60°. Spindle motors transferred tension forces by a cable-pulley on human cadaveric humeri. A six-degree-of-freedom force transducer was mounted directly behind the polyethylene glenoid to measure shear and compressive joint reaction force and calculate the instability ratio (ratio of shear and compressive joint reaction force) with the different force ratios of the deltoid and supraspinatus muscles (2:1 and 1:1). A stepwise change in the inclination by 5° increments allowed simulation of a critical shoulder angle range of 20° to 45°. FINDINGS Tilting the glenoid to cranial (increasing the critical shoulder angle) increases the shear joint reaction force and therefore the instability ratio. A balanced force ratio (1:1) between the deltoid and the supraspinatus allowed larger critical shoulder angles before cranial subluxation occurred than did the deltoid-dominant ratio (2:1). INTERPRETATION Glenoid inclination-dependent changes of the critical shoulder angle have a significant impact on superior glenohumeral joint stability. The increased compensatory activity of the rotator cuff to keep the humeral head centered may lead to mechanical overload and could explain the clinically observed association between large angles and degenerative rotator cuff tears.

Na 1 Nachlass Max Horkheimer, 44 - Korrespondenzen u.a. mit Marthe Roth (p. I 21, 313-463)

2 Briefe und 1 Lebenslauf von Max Horkheimer an Arthur Rosenberg, 1939, 1941; 2 Briefe zwischen Kurt Rosenfeld und Karl Brandt, 22.04.1937, 27.04.1937; 5 Briefe von Kurt Rosenfeld an Max Horkheimer, 1937-19378; 4 Brief und Beilage an Kurt Rosenfeld, 1937-1943; 11 Briefe zwischen Hans W. Rosenhaupt und Max Horkheimer, 1935, 1941, 1942, 1947; 4 Briefe zwischen Samuel I. Roseman und Max Horkheimer, 1939, 03.01.1940; 2 Briefe zwischen J. Rosenstock und Max Horkheimer, 15.07.1946; 2 Briefe zwischen Joseph Adolphe Rosenthal und Max Horkheimer, 09.04.1941, 08.05.1941, sowie Briefwechsel mit Sophie Ries; 2 Briefe zwischen Sophie Ries und Max Horkheimer, 08.05.1941, 11.05.1941; 1 Brief von Max Horkheimer an Lore Woedthke, 08.05.1941; 2 Briefe zwischen Morris Rosenthal und Max Horkheimer, 01.10.1935, 04.10.1935; 1 Brief von Max Horkheimer an das Rosenwald Capital Outlay Fund New York, 30.01.1940; 1 Brief B. Lifschitz an Marthe Roth, 21.04.1937; 1 Brief von Chamorel et Simond an Marthe Roth, 11.06.1937; 1 Brief von F.K. Sung an Marthe Roth, 24.06.1937; 12 Briefe zwischen Marthe Roth und Max Horkheimer, Juli 1937-1938, sowie Briefwechsel mit Louis Vogt; 4 Briefe zwischen Louis Vogt und Max Horkheimer, 10.08.1937, 1937; 1 Brief von Max Horkheimer an Dr. Rothen, 31.01.1935; 1 Umzugsmitteilung von Hans Rothmann; 2 Briefe zwischen Richard C. Rothschild und Max Horkheimer, 11.05.1940, 13.05.1940; 4 Briefe zwischen Ludwig Rothschild, Hilde Rothschild und Max Horkheimer, 1936-15.09.1939; 2 Briefe zwischen S. Rothschildt und Max Horkheimer, 23.11.1940, 29.11.1940; 4 Brief zwischen J. S. Roucek und Max Horkheimer, 1941; 1 Brief von Joseph Rovan an Max Horkheimer, 11.05.1948; 2 Brief zwischen Wilmina Rowland und Max Horkheimer, 13.03.1949, 11.04.1949; 2 Briefe zwischen dem Royal Automobile Club und Max Horkheimer, 26.08.1937, 22.09.1937; 2 Briefe zwischen Royal Motors Inc. und Max Horkheimer, 05.02.1940, 06.03.1940; 1 Beitrag von Nina Rubinstein zur Soziologie des Fremden; 1 Brief von Theodor W. Adorno an Rudd, 09.09.1940; 1 Brief von Jay Rumney an Goldstein, 18.06.1936; 20 Briefe und Beilage zwischen Jay Rumney und Max Horkheimer, 1934- 1937, 1949 sowie Briefwechsel mit D. Mitrany; 3 Briefe zwischen D. Mitrany und Max Horkheimer, 01.12.1937, 1937; 3 Briefe von Theodor W. Adorno an Dagobert D. Runes, 1941; 1 Brief und 1 Beilage von N. Waterman an Georg Rusche, 03.05.1939; 12 Briefe und Beilage zwischen Georg Rusche und Max Horkheimer, 1939-1942 sowie Briefwechsel mit N. Waterman; 1 Brief von N. Waterman an Georg Rusche, 03.04.1939; 2 Briefe zwischen N. Waterman und Max Horkheimer, 21.04.1939, 05.05.1939; 1 Brief von Ruth an Max Horkheimer;

Na 1 Nachlass Max Horkheimer, 578 - Korrespondenzen mit Friedrich (Frederick) Pollock (p. VI 33, 1-360)

1 Brief von Margot von Mendelssohn an Alice H. Maier, 31.12.1942; 1 Drucksache von Fortune [amerikanische Zeitschrift], Dezember 1942; 1 Brief von Frederick Pollock an Bay District Motors Co. (Santa Monica), 17.09.1942; 3 Briefe zwischen Robert M. MacIver und Frederick Pollock, 1943; 2 Briefe zwischen Frederick Pollock und David Rosenblum, 1943; 1 Brief von Robert S. Lynd an Frederick Pollock, 26.04.1943; 1 Brief von Sheed and Ward Inc. (New York) an Max Horkheimer, 08.02.1943; 1 Telegramm von Juliane Favez an Frederick Pollock, 06.02.1943; 1 Brief von Max Horkheimer an das Federal Bureau of Investigation (Los Angeles), 13.01.1943; 1 Brief von Hannah Tillich an Frederick Pollock, 11.01.1943;

Evaluación de metales pesados en suelos de los oasis irrigados de la Provincia de Mendoza : concentraciones totales de Zn, Pb, Cd y Cu

En Mendoza, Argentina, no existen antecedentes respecto de la presencia de elementos trazas, totales y disponibles, relacionados con el uso de los suelos en los oasis irrigados. El objetivo del trabajo, en esta etapa, fue determinar los contenidos totales de plomo (Pb), cadmio (Cd), cinc (Zn) y cobre (Cu) en la capa superficial de suelos (0-25 cm), diferenciados en siete tipos según una clasificación utilitaria: suelos vírgenes (SV); suelos de banquina (SB); suelos vecinos a banquina (SVB); suelos de agricultura intensiva (SAI); suelos de agricultura protegidos por lucha antigranizo (SLAG); suelos afectados por actividad industrial (SI) y suelos urbanos (SU). Sobre un total de 200 muestras se efectuó una digestión ácida en caliente y en los extractos se determinaron los metales en su fracción total, mediante espectrofotometría de absorción atómica (AAS). El análisis estadístico de los datos muestra que los niveles más elevados de Cu y Cd se detectan en SAI, con medias de 39,3 y 2,5 mg kg-1 respectivamente. En SI se observan los mayores valores de Pb, con una media de 80,6 mg kg-1 y en SU los mayores tenores de Zn, con un valor medio de 740 mg kg-1. La Ciudad de Mendoza, con mayor densidad poblacional, presentó los mayores contenidos de Zn, Pb y Cd. Las concentraciones encontradas se ubican por debajo de las exigencias de la legislación argentina y la mayoría de los suelos pueden clasificarse como no contaminados (SNC) o ligeramente contaminados (SLC). Se prevé completar este estudio con la determinación de las fracciones disponibles de los elementos estudiados, correlacionándolos con variables edáficas físico-químicas como textura, pH y materia orgánica.

Thermal behaviour of Sunrise, a balloon-borne solar Telescope

Sunrise is a solar telescope, successfully flown in June 2009 with a long duration balloon from the Swedish Space Corporation Esrange launch site. The design of the thermal control of SUNRISE was quite critical because of the sensitivity to temperature of the optomechanical devices and the electronics. These problems got more complicated due the size and high power dissipation of the system. A detailed thermal mathematical model of SUNRISE was set up to predict temperatures. In this communication the thermal behaviour of SUNRISE during flight is presented. Flight temperatures of some devices are presented and analysed. The measured data have been compared with the predictions given by the thermal mathematical models. The main discrepancies between flight data and the temperatures predicted by the models have been identified. This allows thermal engineers to improve the knowledge of the thermal behaviour of the system for future missions.

A method for Kinematic Calibration of a Parallel Robot by using one camera in hand and a spherical object

The main purpose of robot calibration is the correction of the possible errors in the robot parameters. This paper presents a method for a kinematic calibration of a parallel robot that is equipped with one camera in hand. In order to preserve the mechanical configuration of the robot, the camera is utilized to acquire incremental positions of the end effector from a spherical object that is fixed in the word reference frame. The positions of the end effector are related to incremental positions of resolvers of the motors of the robot, and a kinematic model of the robot is used to find a new group of parameters which minimizes errors in the kinematic equations. Additionally, properties of the spherical object and intrinsic camera parameters are utilized to model the projection of the object in the image and improving spatial measurements. Finally, the robotic system is designed to carry out tracking tasks and the calibration of the robot is validated by means of integrating the errors of the visual controller.

Performance optimization in switched reluctance motor drives

In this paper, switched reluctance motors (SRM) are proposed as an alternative for electric power assisted steering (EPAS) applications. A prototype machine has been developed as very attractive design for a steering electric motor, both from a cost and size perspective. A fourphase 8/6 SRM drive is designed for a rack type EPAS which should provide a maximum force of 10 kN. Two-dimension finite element analysis is used to validate the design.

Kinematic analysis of a novel 2-d.o.f. orientation device

This paper presents the development of a new parallel robot designed for helping with bone milling surgeries. The robot is a small modular wrist with 2 active degrees of freedom, and it is proposed to be used as an orientation device located at the end of a robotic arm designed for bone milling processes. A generic kinematic geometry is proposed for this device. This first article shows the developments on the workspace optimization and the analysis of the force field required to complete a reconstruction of the inferior jawbone. The singularities of the mechanism are analyzed, and the actuator selection is justified with the torque requirements and the study of the force space. The results obtained by the simulations allow building a first prototype using linear motors. Bone milling experiment video is shown as additional material.

Numerical Model of a Variable-Combined-Cycle Engine for Dual Subsonic and Supersonic Cruise

Efficient high speed propulsion requires exploiting the cooling capability of the cryogenic fuel in the propulsion cycle. This paper presents the numerical model of a combined cycle engine while in air turbo-rocket configuration. Specific models of the various heat exchanger modules and the turbomachinery elements were developed to represent the physical behavior at off-design operation. The dynamic nature of the model allows the introduction of the engine control logic that limits the operation of certain subcomponents and extends the overall engine operational envelope. The specific impulse and uninstalled thrust are detailed while flying a determined trajectory between Mach 2.5 and 5 for varying throttling levels throughout the operational envelope.

Simulation, Design and Analysis of Air-Breathing Combined-Cycle Engines for High Speed Propulsion

Desde la aparición del turborreactor, el motor aeróbico con turbomaquinaria ha demostrado unas prestaciones excepcionales en los regímenes subsónico y supersónico bajo. No obstante, la operación a velocidades superiores requiere sistemas más complejos y pesados, lo cual ha imposibilitado la ejecución de estos conceptos. Los recientes avances tecnológicos, especialmente en materiales ligeros, han restablecido el interés por los motores de ciclo combinado. La simulación numérica de estos nuevos conceptos es esencial para estimar las prestaciones de la planta propulsiva, así como para abordar las dificultades de integración entre célula y motor durante las primeras etapas de diseño. Al mismo tiempo, la evaluación de estos extraordinarios motores requiere una metodología de análisis distinta. La tesis doctoral versa sobre el diseño y el análisis de los mencionados conceptos propulsivos mediante el modelado numérico y la simulación dinámica con herramientas de vanguardia. Las distintas arquitecturas presentadas por los ciclos combinados basados en sendos turborreactor y motor cohete, así como los diversos sistemas comprendidos en cada uno de ellos, hacen necesario establecer una referencia común para su evaluación. Es más, la tendencia actual hacia aeronaves "más eléctricas" requiere una nueva métrica para juzgar la aptitud de un proceso de generación de empuje en el que coexisten diversas formas de energía. A este respecto, la combinación del Primer y Segundo Principios define, en un marco de referencia absoluto, la calidad de la trasferencia de energía entre los diferentes sistemas. Esta idea, que se ha estado empleando desde hace mucho tiempo en el análisis de plantas de potencia terrestres, ha sido extendida para relacionar la misión de la aeronave con la ineficiencia de cada proceso involucrado en la generación de empuje. La metodología se ilustra mediante el estudio del motor de ciclo combinado variable de una aeronave para el crucero a Mach 5. El diseño de un acelerador de ciclo combinado basado en el turborreactor sirve para subrayar la importancia de la integración del motor y la célula. El diseño está limitado por la trayectoria ascensional y el espacio disponible en la aeronave de crucero supersónico. Posteriormente se calculan las prestaciones instaladas de la planta propulsiva en función de la velocidad y la altitud de vuelo y los parámetros de control del motor: relación de compresión, relación aire/combustible y área de garganta. ABSTRACT Since the advent of the turbojet, the air-breathing engine with rotating machinery has demonstrated exceptional performance in the subsonic and low supersonic regimes. However, the operation at higher speeds requires further system complexity and weight, which so far has impeded the realization of these concepts. Recent technology developments, especially in lightweight materials, have restored the interest towards combined-cycle engines. The numerical simulation of these new concepts is essential at the early design stages to compute a first estimate of the engine performance in addition to addressing airframe-engine integration issues. In parallel, a different analysis methodology is required to evaluate these unconventional engines. The doctoral thesis concerns the design and analysis of the aforementioned engine concepts by means of numerical modeling and dynamic simulation with state-of-the-art tools. A common reference is needed to evaluate the different architectures of the turbine and the rocket-based combined-cycle engines as well as the various systems within each one of them. Furthermore, the actual trend towards more electric aircraft necessitates a common metric to judge the suitability of a thrust generation process where different forms of energy coexist. In line with this, the combination of the First and the Second Laws yields the quality of the energy being transferred between the systems on an absolute reference frame. This idea, which has been since long applied to the analysis of on-ground power plants, was extended here to relate the aircraft mission with the inefficiency of every process related to the thrust generation. The methodology is illustrated with the study of a variable- combined-cycle engine for a Mach 5 cruise aircraft. The design of a turbine-based combined-cycle booster serves to highlight the importance of the engine-airframe integration. The design is constrained by the ascent trajectory and the allocated space in the supersonic cruise aircraft. The installed performance of the propulsive plant is then computed as a function of the flight speed and altitude and the engine control parameters: pressure ratio, air-to-fuel ratio and throat area.

On the formation of nitrogen oxides in the combustion processes of hydrogen in air

A research programme is being carried out at the Institute Nacional de Tecnica Aeroespacial of Spain, on several aspects of the formation of nitrogen oxides in continuous flow combustion systems, considering hydrogen and hydrocarbons as fuels. The research programme is fundamentally oriented on the basic aspects of the problem, although it also includes the study of the influence on the formation process of several operational and design variables of the combusters, such as type of fuels, fuel/air ratio, degree of mixing in premixed type flames, existence of droplets as compared with homogeneous combustion.This problem of nitrogen oxides formation is receiving lately great attention, specially in connection with automobile reciprocating engines and aircraft gas turbines. This is due to the fact of the increasing frequency and intensity of photochemical hazes or smog, typical of urban areas submitted to strong solar radiation, which are originated by the action on organic compounds of the oxidants resulting from the photochemical decomposition of nitrogen dioxide N02. In the combustion process almost all nitrogen oxides are in form of NO. This nitric oxide reacts with the oxygen of the air and forms N02, this reaction only taking place in or near the exhaust of tne motors, since the N0-02 reaction becomes frozen for the concentration existing in the atmosphere.

Testing equipment for the improvement of mechanical devices to minimize damage to fruit in commercial packing lines.

Damages -reduced in fruit packing lines is a major cause of grace reduction and quality loos in fresh marks: fruit. Fruit must be treated gently during in sir handling to improve their qualityin order to get a good price in a competitive market. The correct post-hardvest handling in fruit packing lines is a prerequisite to cut down the heavy post-harvest losses. Fruit packing lines must be evaluated, studying their design, the impacts applied to the fruits, the characteristics of the materials, etc. This study establishes the possibility of carrying out modifications and tests in a packing line during a long period of time. For this purpose, an experimental fruit packing line has been designed and located in the Agricultural Engineering Department of the Polythecnic University of Madrid with the aim of improving mechanical devices and fruit handling conditions to minimize damage to fruit. The experimental line consists of several transporting belts, one rollers transporter, one sizer, one elevator, one singularizer, and three trays to receive the calibrated fruit. The line has a length of 6.15 m and a width cf 1.9 m. Movement of the different components is regulated by electric motors with variable velocity electronically controlled. The height of the transfer points is variable and can be easily modified. The experimental line has been calibrated using two instrumented spheres IS 100 (8.8 cm Ø and6.2cm Ø). Average acceleration values obtained in all the transfers of the experimental line lay under 80 g's, although there is big variation for some of them being some values above 100 g's.