Overview of the new concurrent engineering facility at DLR

H Schumann, A Braukhane, A Gernd, JT Grundmann… - 2008 - elib.dlr.de
In October 2008, the German Aerospace Center (DLR) inaugurated a new Concurrent
Engineering Facility (CEF) in Bremen which is used mainly for design studies at the new …

Collaborative satellite configuration supported by interactive visualization

PM Fischer, R Wolff, A Gerndt - 2012 IEEE Aerospace …, 2012 - ieeexplore.ieee.org
Planning a spacecraft requires the expert knowledge from diverse disciplines, such as
propulsion or structure. Reliable communication between the experts is crucial, as the …

Variability-Aware Design of Space Systems: Variability Modelling, Configuration Workflow and Research Directions

S Lazreg, V Bohlachov, L Rana, A Hein… - Proceedings of the 16th …, 2022 - dl.acm.org
Designing spacecraft such as satellites is known as an extremely difficult problem. It requires
complex decision making at different concerns from mission requirements to system …

Trend of European Spacecraft Simulator Development

H Lee - Current Industrial and Technological Trends in …, 2008 - koreascience.kr
As the cost of the operational spacecraft simulator is a large portion of the spacecraft cost
and its requirements increase, it is given the pressures to reduce the cost and the …

유럽우주비행체시뮬레이터연구개발동향

이훈희 - 항공우주산업기술동향, 2008 - dbpia.co.kr
유럽의 우주비행체 시뮬레이터는 요구사항의 증가와 함께 우주비행체 개발 비용에서 높은
비율을 차지하여 개발 비용 절감과 개발 기간 단축의 압력에 직면하고 있다. 현재 유럽은 …

[PDF][PDF] Integrated Spacecraft Design: Demonstration of a prototype process and platform for satellite design application

L Rana, V Bohlachov, A Hein - Proceedings of International …, 2022 - orbilu.uni.lu
Conceptual Design (CD) is one of the most critical life-cycle phases where crucial design
decisions are taken and a baseline design is frozen. A traditional CD approach applies a …

Automatic code generation for attitude and orbit control systems using domain-specific languages

PA Isidro - 2014 - elib.dlr.de
The Attitude and Orbit Control System (AOCS) is the spacecraft subsystem responsible for
determining and controlling the vehicle's orbit and orientation. Similarly to other kinds of …

[PDF][PDF] Gekoppelte Ausführung von Simulink-und Modelica-Modellen mittels SMP2

A Röhnsch - 2009 - roehnsch.de
Übersteigt die Gröÿe eines Simulationsmodells die Möglichkeiten eines Modellierers,
müssen mehrere Modellierer zusammen daran arbeiten. Dazu wird das Modell aufgeteilt …

[引用][C] 空间任务概念设计阶段的协同工作环境

邓丽, 杨震, 彭晓东 - 无线电工程, 2016