Ritter Homburg vom Hils, oder Rache und Vergeltung : historisch-romantisches Gemälde aus den Zeiten der Kreuzzüge

von F. Th. Wangenheim

Elfas und Ahlsburg - die Struktur der Schollengrenze zwischen Hils und Solling

The Elfas, Ahlsburg, and Salzderhelden overthrusts have been considered for a long time to be halotectonic structures caused by diapiric rise of Zechstein salt into thrust planes and other zones of weakness in the overlying rocks. Much of the Markoldendorf syncline between the overthrusts is covered by Quaternary deposits. The structure of the syncline and its western and southern boundaries were mapped with the help of many boreholes and micropalaeontological dating during remapping of the 1 : 25 000 geological sheet 4124 (Dassel). The Ahlsburg overthrust has now been shown to continue to the NW and to lead into the Lüthorst graben, which truncates the syncline in the west and passes into the crestal fault of the Elfas anticline. Figure 6 shows the NW-SE trending faults bounding three blocks which, according to seismic interpretation (Geotectonic Atlas 1996), have moved several times, in some areas in opposite senses. The NNE-SSW-trending grabens act as hinges, separating the NW-SE faults into sections that have undergone different movement.

Robust flight stability and control for micro air vehicles.

This chapter presents the real time validation of fixed order robust 112 controller designed for the lateral stabilisation of a micro air vehicle named Sarika2. Digital signal processor (DSP) based onboard computer named flight instrumentation controller (FIC) is designed to operate under automatic or manual mode. FIC gathers data from multitude of sensors and is capable of closed loop control to enable autonomous flight. Fixed order lateral H-2 controller designed with the features such as incorporation of level I flying qualities, gust alleviation and noise rejection is coded on to the FIC. Challenging real time hardware in loop simulation (HILS) is done with dSPACE1104 RTI/RTW. Responses obtained from the HILS are compared with those obtained from the offline simulation. Finally, flight trials are conducted to demonstrate the satisfactory performance of the closed loop system. The generic design methodology developed is applicable to all classes of Mini and Micro air vehicles.

SeP hole injection layer for devices based on organic materials

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)