Abstract: The invention describes the use of deoxyspergualin (DSG) or an analogue thereof for the preparation of a medicament for the treatment of and/or prophylaxis against hyperreactive inflammatory diseases and autoimmune diseases, wherein the treatment is performed in cycles.

Abstract: A low-altitude flight guidance system for an aircraft including a warning generator that generates a warning based upon a predicted position. The system further including a first sensor system having a terrain database and a calculation module that determines a current position of the aircraft with respect to terrain stored in the terrain database and that determines a reference altitude hDB of the terrain at the current position. The system further includes a second sensor system and a module that determines a predetermined flight altitude difference ?hF at the predicted position and terrain data in a region U of the predicted position. Moreover, the system includes an altitude prediction module that predicts an altitude and forwards the predicted altitude to the warning generator. The warning is based upon the aircraft reaching, approaching, or exceeding a warning altitude limit, and the altitude prediction module determination for the predicted position is based upon a prediction set point.

Abstract: The invention describes the use of deoxyspergualin (DSG) or an analogue thereof for the preparation of a medicament for the treatment of and/or prophylaxis against hyperreactive inflammatory diseases and autoimmune diseases, wherein the treatment is performed in cycles.

Abstract: The invention describes the use of deoxyspergualin (DSG) or an analogue thereof for the preparation of a medicament for the treatment of and/or prophylaxis against hyperreactive inflammatory diseases and autoimmune diseases, wherein the treatment is performed in cycles.

Abstract: A low-altitude flight guidance system for an aircraft including a warning generator that generates a warning based upon a predicted position. The system further including a first sensor system having a terrain database and a calculation module that determines a current position of the aircraft with respect to terrain stored in the terrain database and that determines a reference altitude hDB of the terrain at the current position. The system further includes a second sensor system and a module that determines a predetermined flight altitude difference ?hF at the predicted position and terrain data in a region U of the predicted position. Moreover, the system includes an altitude prediction module that predicts an altitude and forwards the predicted altitude to the warning generator. The warning is based upon the aircraft reaching, approaching, or exceeding a warning altitude limit, and the altitude prediction module determination for the predicted position is based upon a prediction set point.

Abstract: A method and apparatus for recognizing a crash, in a vehicle by measuring vehicle speed change continuously within a limited time periods and comparing the measured values with those determined in prior time periods. Acceleration can be differentiated out by means of the above-mentioned process/arrangement and can be evaluated if, in the case of a high-speed and low-speed crash, it should not be possible to differentiate sufficiently by means of the partial speed difference. Different partial speed differences (by means of observation periods of different durations) can be measured and compared in order to permit ignition in the case of slower (oblique) crashes only within a limited time window in the initial phase of the crash.