@InProceedings{SantosRocBogBenRem:2015:NoSoSp,
author = "Santos, Willer Gomes dos and Rocco, Evandro Marconi and Boge,
Toralf and Benninghoff, Heike and Rems, Florian",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {German Aerospace
Center (DLR)} and {German Aerospace Center (DLR)} and {German
Aerospace Center (DLR)}",
title = "A novel solution for the spacecraft mixed actuators problem based
on a multiobjective optimization method",
booktitle = "Proceedings...",
year = "2015",
organization = "International Symposium on Space Flight Dynamics, 25.",
keywords = "Mixed Actuators Problem, Multiobjective Optimization, Final
Approach Rendezvous.",
abstract = "In this paper, a novel solution for the mixed actuators problem is
proposed. This approach uses a multiobjective optimization
technique for commanding a group of actuators (thrusters, reaction
wheels and magnetic torqrods) simultaneously optimizing a set of
objective functions. The multiobjective problem is formulated
using combinatorial combinations of the control signal for
composing the decision space. The proposed model, called Actuator
Multiobjective Command Method (AMCM), is included in a complete
guidance, navigation and control loop applied to the final
approach rendezvous scenario. Its performance, compared to
different actuators configurations, has been evaluated in
numerical simulations. In addition, AMCM has been integrated and
tested in the hardware-in-the-loop rendezvous and docking
simulator of the German Aerospace Center. Results have indicated
effectiveness and robustness in both purely numerical and
real-time simulations.",
conference-location = "Munich, Germany",
conference-year = "19-23 Oct.",
language = "en",
urlaccessdate = "15 jun. 2024"
}