Refine
Year of publication
- 2019 (194) (remove)
Institute
- Fachbereich Medizintechnik und Technomathematik (64)
- IfB - Institut für Bioengineering (40)
- Fachbereich Luft- und Raumfahrttechnik (38)
- Fachbereich Elektrotechnik und Informationstechnik (30)
- INB - Institut für Nano- und Biotechnologien (20)
- Fachbereich Energietechnik (19)
- Fachbereich Maschinenbau und Mechatronik (16)
- Fachbereich Chemie und Biotechnologie (11)
- Fachbereich Bauingenieurwesen (8)
- MASKOR Institut für Mobile Autonome Systeme und Kognitive Robotik (8)
Language
- English (194) (remove)
Document Type
- Article (95)
- Conference Proceeding (74)
- Part of a Book (15)
- Book (4)
- Doctoral Thesis (3)
- Conference: Meeting Abstract (2)
- Talk (1)
Keywords
- Enterprise Architecture (2)
- Seismic design (2)
- Achilles tendon (1)
- Advanced driver assistance systems (ADAS/AD) (1)
- Aircraft design (1)
- Analytics (1)
- Architectural gear ratio (1)
- Assistive technology (1)
- Automatic control (1)
- BEV (1)
- Case Study (1)
- Change Management (1)
- Combustion (1)
- Components (1)
- Corporate Culture (1)
- Correlations (1)
- Decentral (1)
- Design examples (1)
- Design rules (1)
- Digital Age (1)
- Diversity Management (1)
- Drag (1)
- Earthquake (1)
- Emilia-Romagna earthquake (1)
- Empirical consequence curves (1)
- Empirical fragility functions (1)
- Engineering (1)
- Engineering optimization (1)
- Eurocode 8 (1)
- Force (1)
- Gearbox (1)
- Geometry (1)
- Goodness-of-fit test (1)
- Graph Theory (1)
- Green aircraft (1)
- Gust wind response (1)
- Human-Computer interaction (1)
- Hybrid-electric aircraft (1)
- Hydrogen (1)
- ISO 26262 (1)
- In-plane (1)
- Industrial units (1)
- Innovation Management (1)
- Isolation (1)
- Iterative learning control (1)
- Knee (1)
- Load modeling (1)
- Low NOx (1)
- Low emission (1)
- Machine learning (1)
- Mechanical (1)
- Mixed-integer nonlinear black-box optimization (1)
- Multi-sample problem (1)
- On-site (1)
- Optimization (1)
- Out-of-plane (1)
- PBEE (1)
- Parametric bootstrap (1)
- Powertrain (1)
- Pre-treatment (1)
- Precast buildings (1)
- Preface (1)
- Product family optimization (1)
- Pushover analysis (1)
- Rehabilitation engineering (1)
- Resilience Assessment (1)
- Response spectrum (1)
- Robotic Process Automation (1)
- Running (1)
- Safety of the intended functionality (SOTIF) (1)
- Safety-critical systems validation (1)
- Seismic (1)
- Silos (1)
- Software Robots (1)
- Spectral analysis (1)
- Statistics (1)
- Stiffness (1)
- Tanks (1)
- Tendon properties (1)
- Training (1)
- Unmanned Air Vehicle (1)
- Volume of confidence regions (1)
- WLTP (1)
- Water Supply System (1)
- Wind turbulence (1)
- asymptotic relative efficiency (1)
- concentrating collector (1)
- frequency mixing magnetic detection (1)
- likelihood ratio test (1)
- magnetic actuation (1)
- magnetic sandwich immunoassay (1)
- magnetic separation (1)
- magnetic tweezers (1)
- magnetophoretic velocity (1)
- multinomial distribution (1)
- multiparametric immunoassays (1)
- multivariate normal distribution (1)
- point-focussing system (1)
- raytracing (1)
- responsive space (1)
- small solar system body characterisation (1)
- small spacecraft asteroid lander (1)
- small spacecraft solar sail (1)
- solar process heat (1)
- superparamagnetic bead (1)
- system engineering (1)
20 years after the successful ground deployment test of a (20 m) 2 solar sail at DLR Cologne, and in the light of the upcoming U.S. NEAscout mission, we provide an overview of the progress made since in our mission and hardware design studies as well as the hardware built in the course of our solar sail technology development. We outline the most likely and most efficient routes to develop solar sails for useful missions in science and applications, based on our developed `now-term' and near-term hardware as well as the many practical and managerial lessons learned from the DLR-ESTEC Gossamer Roadmap. Mission types directly applicable to planetary defense include single and Multiple NEA Rendezvous ((M)NR) for precursor, monitoring and follow-up scenarios as well as sail-propelled head-on retrograde kinetic impactors (RKI) for mitigation. Other mission types such as the Displaced L1 (DL1) space weather advance warning and monitoring or Solar Polar Orbiter (SPO) types demonstrate the capability of near-term solar sails to achieve asteroid rendezvous in any kind of orbit, from Earth-coorbital to extremely inclined and even retrograde orbits. Some of these mission types such as SPO, (M)NR and RKI include separable payloads. For one-way access to the asteroid surface, nanolanders like MASCOT are an ideal match for solar sails in micro-spacecraft format, i.e. in launch configurations compatible with ESPA and ASAP secondary payload platforms. Larger landers similar to the JAXA-DLR study of a Jupiter Trojan asteroid lander for the OKEANOS mission can shuttle from the sail to the asteroids visited and enable multiple NEA sample-return missions. The high impact velocities and re-try capability achieved by the RKI mission type on a final orbit identical to the target asteroid's but retrograde to its motion enables small spacecraft size impactors to carry sufficient kinetic energy for deflection.
Wind loads have great impact on many engineering structures. Wind storms often cause irreparable damage to the buildings which are exposed to it. Along with the earthquakes, wind represents one of the most common environmental load on structures and is relevant for limit state design. Modern wind codes indicate calculation procedures allowing engineers to deal with structural systems, which are susceptible to conduct wind-excited oscillations. In the codes approximate formulas for wind buffeting are specified which relate the dynamic problem to rather abstract parameter functions. The complete theory behind is not visible in order to simplify the applicability of the procedures. This chapter derives the underlying basic relations of the spectral method for wind buffeting and explains the main important applications of it in order to elucidate part of the theoretical background of computations after the new codes. The stochasticity of the wind processes is addressed, and the analysis of analytical as well as measurement based power spectra is outlined. Short MATLAB codes are added to the Appendix 3 which carry out the computation of a single sided auto-spectrum from a statistically stationary, discrete stochastic process. Two examples are presented.
The utilization of phase change material (PCM) for latent heat storage and thermal control of spacecraft has been demonstrated in the past in few missions only. One limiting factor was the fact that all concepts developed so far envisioned the PCM to be applied as an additional capacitor, encapsulated in its own housing, leading to mass, efficiency and accommodation challenges. Recently, the application of PCM within the scan cavity of a GEOS type satellite has been suggested, in order to tackle thermal issues due to direct sun intrusion (Choi, M., 2014). However, the application of PCM in such complex mechanical structures is extremely challenging. A new concept to tackle this issue is currently under development at the FH Aachen University of Applied Sciences. The concept "Infused Thermal Solutions (ITS)" is based on the idea to 3D print metallic structures in their regular functional shape, but double walled with internal lattice support structures, allowing the infusion of a PCM layer directly into the voids and eliminating the need for additional parts and interfaces. Together with OHB System, FH Aachen theoretically studied the application of this technology to the Meteosat Third Generation (MTG) Infra-Red Sounder (IRS) instrument. The study focuses on the scan cavity and entrance baffling assembly (EBA) of the IRS. It consists of thermal analyses, 3D-redesign and bread boarding of a scaled and PCM infused EBA version. In the thermal design of the alternative EBA, PCM was applied directly into the EBA, simulating the worst hot case sun intrusion of the mission. By applying 4kg of PCM (to a 60kg baffle) the EBA temperature excursions during sun intrusion were limited from 140K to 30K, leading to a significant thermo-opto-elastic performance gain. This paper introduces the ITS concept development status.