Refine
Year of publication
- 2009 (62) (remove)
Document Type
- Conference Proceeding (20)
- Article (unreviewed) (16)
- Part of a Book (7)
- Book (6)
- Article (reviewed) (5)
- Patent (3)
- Contribution to a Periodical (2)
- Periodical Part (1)
- Report (1)
- Study Thesis (1)
Conference Type
- Konferenzartikel (14)
- Konferenz-Poster (3)
- Sonstiges (3)
- Konferenz-Abstract (1)
Has Fulltext
- no (62) (remove)
Is part of the Bibliography
- yes (62)
Keywords
- Dünnschichtchromatographie (2)
- 2D-Ortung (1)
- 3D User Interface (1)
- 3D-Ortung (1)
- Absorption (1)
- Abwärmenutzung (1)
- Akustik (1)
- Alexander von Humboldt (1)
- Android (1)
- Belastung (1)
Institute
Open Access
- Closed Access (20)
- Open Access (16)
- Bronze (6)
- Closed (3)
There are additional long-term effects which also change the micro-structure of the polymer network and consequently the effective number of polymer chains in the material. These effects are summarized by ageing processes and will be used in the following to explain the basic assumptions of the model which can be generalized to simulate the viscous behaviour of the material. An implementation of these concepts into FEM codes is straightforward and has been carried out to the solver ABAQUS, Baaser & Ziegler (2006), Baaser et al. (2009).
Energietechnik
(2009)
Dieses Lehrbuch vermittelt dem Leser ein grundlegendes Verständnis für die Zusammenhänge der Energieumwandlungsprozesse. Es umfasst die gesamte Bandbreite der Energietechnik. Die Schwerpunkte reichen von nachhaltigen, erneuerbaren Energietechniken, Kombianlagen (z. B. Gas- und Dampfturbinen-Kraftwerke) über Anlagen mit Kraft-Wärme-Kälte-Kopplung bis hin zum Kyoto-Protokoll. Die 4. Auflage beinhaltet erstmals Übungsaufgaben mit ausführlichen Lösungen zu den einzelnen Kapiteln. Mehrere Kapitel sind aktualisiert. Das Kapitel 18 „Liberalisierung der Energiemärkte“ ist neu gefasst.
'Natural Sound'
(2009)
Grundkurs Regelungstechnik
(2009)
Komprimierte, mathematisch ausgerichtete Einführung in Grundlagen der Regelungstechnik für Studierende der Ingenieurwissenschaften an Fachhochschulen und Universitäten. Neuausgabe von "Kompaktkurs Regelungstechnik" (ID 17/02), die um ca. 50 Seiten erweitert (Abschnitt über betriebliche Systeme) und durchgehend aktualisiert wurde. Ist jetzt auf Bachelorstudiengänge ausgerichtet und enthält zahlreiche Übungsaufgaben und durchgerechnete Beispiele. Die alte Ausgabe sollte ersetzt werden.
An interlaboratory comparison was carried out to evaluate the effectiveness of a method based on HPTLC in which reagent-free derivatization is followed by UV/fluorescence detection. The method was tested for the determination of sucralose (C12H19C13O8; (2R,3R,4R,5S,6R)-2-[(2R,3S,4S,5S)-2,5-bis(chloromethyl)-3,4-dihydroxyoxolan-2-yl]oxy-5-chloro-6-hydroxymethyl)oxane-3, 4-diol; CAS Registry No. 56038-13-2) in carbonated and still beverages at the proposed European regulatory limits. For still beverages, a portion of the sample was diluted with methanol-water. For carbonated beverages, a portion of the sample was degassed in an ultrasonic bath before dilution. Turbid beverages were filtered after dilution through an HPLC syringe filter. The separation of sucralose was performed by direct application on amino-bonded (NH2) silica gel HPTLC plates (no cleanup needed) with the mobile phase acetonitrile-water. Sucralose was determined after reagent-free derivatization at 190 degrees C; it was quantified by measurements of both UV absorption and fluorescence. The samples, both spiked and containing sucralose, were sent to 14 laboratories in five different countries. Test portions of a sample found to contain no sucralose were spiked at levels of 30.5, 100.7, and 299 mg/L. Recoveries ranged from 104.3 to 124.6% and averaged 112% for determination by UV detection; recoveries ranged from 98.4 to 101.3% and averaged 99.9% for determination by fluorescence detection. On the basis of the results for spiked samples (blind duplicates at three levels), as well as sucralose-containing samples (blind duplicates at three levels and one split level), the values for the RSDr ranged from 10.3 to 31.4% for determinations by UV detection and from 8.9 to 15.9% for determinations by fluorescence detection. The values for the RSDR values ranged from 13.5 to 31.4% for determinations by UV detection and from 8.9 to 20.7% for determinations by fluorescence detection.
In the recent two years the authors have developed a light weight and low power flight control system for model helicopters consisting of an attitude and heading reference system (AHRS), a navigator (INS) augmented with GPS, barometric altitude sensor and a magnetic sensor, a flight control computer (FCC) and bidirectional ground data links. The system has been tested on a commercial stunt flight model helicopter. The AHRS consists of three MEMS-gyros, two 2-axis MEMS accelerometers and a microcontroller performing the required sensor compensation and data processing to generate attitude angles and true rate and acceleration data of the flying platform. The heading angle is augmented with a 2-axis magnetic sensor. The AHRS is stunt flight capable. The INS integrates the acceleration data to obtain velocity and position data. All data are calculated in both the helicopter and the local earth frame with 50 Hz rate. The algorithm is augmented with GPS data for the lateral movement and with a barometric altitude sensor for the vertical movement. The barometric data are compensated for air pressure changes due to the helicopter main rotor. The FCC contains a set of control loops in order to stabilize the helicopter in all axis and to perform commanded velocity and position tasks. The sampling rate for the control loops is again 50 Hz allowing flight control with high bandwidth. Various safety features are implemented in the software. The bidirectional data link is based on a 2.4 GHz Bluetooth Class I RF-link with a 115 kbaud data rate. A dipole antenna is used on the helicopter, an automatically tracking patch antenna is used on the ground. For commanded velocity flight a standard 35 MHz RF-link is used. For data sampling, monitoring and mode control a laptop is used on the ground. Several operating modes are implemented ranging from commanded velocity flight to simple automatic stunt flight according to predefined flight tracks. The model helicopter is an ALIGN TREX 600 with 3 kg flight mass and a brushless electric motor. The rotor diameter is 1.40 m. The helicopter is able to carry a payload which mass depends on the size of the installed LiPo-cells and the purpose of the flight mission. The system has been tested in quite a few flight tests and missions. The helicopter is controlled safely up to wind loads of at least 5 Beaufort - 6 Beaufort. Data and video captures will be presented. If permission is granted, a demonstration flight will be performed on the premises of the conference.