Saab Automobile AB

About: Saab Automobile AB is a based out in . It is known for research contribution in the topics: Radar & Signal. The organization has 760 authors who have published 890 publications receiving 11811 citations.

CompSize: Automated Size Estimation of Embedded Software Components

Abstract: Accurate estimation of Software Code Size isimportant for developing cost-efficient embedded systems. TheCode Size affects the amount of system resources needed, likeROM and RAM memory, and processing capacity. In ourprevious work, we have estimated the Code Size based on CFP (COSMIC Function Points) within 15% accuracy, with thepurpose of deciding how much ROM memory to fit intoproducts with high cost pressure. Central in that work is themapping between CFP and the information available early inthe development process. We have previously defined a UMLProfile capturing the information needed for CFPmeasurement and estimation of Code Size. The key idea was toextend UML components to contain all the necessaryinformation. In this paper, we show how we developed a toolfor automated estimation of Code Size based on our UMLProfile. The tool is designed to permit Code Size estimationbased on other UML diagrams than components. A case studyevaluates the UML Profile and the tool in a realistic case.

Study of industrially applied methods for verification, validation and uncertainty quantification of simulator models

Abstract: To better utilize the potential of system simulation models and simulators, industrially applicable methods for Verification, Validation and Uncertainty Quantification (VV&UQ) are crucial. This paper presents an exploratory case study of VV&UQ techniques applied on models integrated in aircraft system simulators at Saab Aeronautics and in driving simulators at the Swedish National Road and Transport Research Institute (VTI). Results show that a large number of Verification and Validation (V&V) techniques are applied, some of which are promising for further development and use in simulator credibility assessment. Regarding the application of UQ, a large gap between academia and this part of industry has been identified, and simplified methods are needed. The applicability of the NASA Credibility Assessment Scale (CAS) at the studied organizations is also evaluated and it can be concluded that the CAS is considered to be a usable tool for achieving a uniform level of V&V for all models included in a simulator, although its implementation at the studied organizations requires tailoring and coordination.

A Ka-Band Active Integrated Antenna for 5G Applications: Initial Design Flow

Abstract: Initial technology and design decisions are presented as part of a design flow to realize an active integrated antenna (array) element for 5G applications at Ka-band. The objective is to synthesize an antenna impedance that directly matches the amplifier optimal load impedance in order to maximize the overall efficiency of the integrated antenna-amplifier system while attaining an output power in the range of 15–25 dBm. A strategy to subsequently co-optimize this combined system is also discussed. Direct matching overcomes the insertion losses and bandwidth limitations of impedance-transforming networks, obviates the use of a standard 50-Ohm reference impedance, and potentially results in more cost-effective, more compact, and better performing active antenna designs in general.

Projectile for the dispersal of a load with time delay

Abstract: A projectile for the dispersal of a load with time delay after firing from a launching tube (1) with hot gas under pressure is described. It comprises a cylindrical casing (2) comprising a cross wall (3) on one side of which there is a first pressure chamber (7) limited outwardly by an external side wall (4), provided with a supply opening (5) for the hot gas. The cross wall (3) limits on its other side a second pressure chamber (9) which is formed by the casing and a piston (8) axially movable in the casing, which stands in connection with said load (10). A throttled gas connection (11) is provided between the first and second pressure chambers (7, 9). The piston (8), under the effect of a pressure built up in the second pressure chamber, is arranged to perform an axial movement, firing the load (10) out of the casing (2), but not until the pressure has reached a predetermined level. The projectile is characterized particularly in that a fibrous material (16) with relatively good thermal conductivity, for instance steel wool, is so arranged in the first pressure chamber (7), that the pressure in the gas conducted to the first pressure chamber remains relatively constant with time, whereby the pressure in the gas conducted to the second pressure chamber (9) shows a relatively constant increase per time unit.

Positioning embedded software maintenance within industrial maintenance

Abstract: Little is known about of how software embedded in complex industrial technical systems is maintained. In this paper, we identify industrial maintenance process steps and position software maintenance activities within them. We do this in the context of JAS 39 Gripen, a multi-role combat aircraft developed by Saab.