Sciweavers

45 search results - page 1 / 9
» An Hybrid Design Solution For Spacecraft Simulators
Sort
View
CAISE
2008
Springer
13 years 6 months ago
An Hybrid Design Solution For Spacecraft Simulators
Abstract. The European Space Agency (ESA) has created the Simulation Model Portability 2 (SMP2) standard with the purpose to provide a design solution for the project of Spacecraft...
Vitor Rodrigues, João Correia Lopes, Ana Mo...
CEC
2010
IEEE
13 years 6 months ago
Constrained global optimization of low-thrust interplanetary trajectories
The optimization of spacecraft trajectories can be formulated as a global optimization task. The complexity of the problem depends greatly on the problem formulation, on the spacec...
Chit Hong Yam, David Di Lorenzo, Dario Izzo
AUTOMATICA
2005
178views more  AUTOMATICA 2005»
13 years 4 months ago
Spacecraft attitude control using explicit model predictive control
In this paper, an explicit model predictive controller for the attitude of a satellite is designed. Explicit solutions to constrained linear MPC problems can be computed by solvin...
Øyvind Hegrenæs, Jan Tommy Gravdahl, ...
ICCD
2007
IEEE
190views Hardware» more  ICCD 2007»
14 years 1 months ago
Hybrid resistor/FET-logic demultiplexer architecture design for hybrid CMOS/nanodevice circuits
Hybrid nanoelectronics are emerging as one viable option to sustain the Moore’s Law after the CMOS scaling limit is reached. One main design challenge in hybrid nanoelectronics ...
Shu Li, Tong Zhang
HYBRID
2004
Springer
13 years 10 months ago
On the Optimal Control of Switch-Mode DC-DC Converters
This paper presents a new solution approach to the optimal control problem of fixed frequency switch-mode DC-DC converters using hybrid systems methodologies. In particular, the n...
Tobias Geyer, Georgios Papafotiou, Manfred Morari