document title / titre du document TRP W ORK PLAN ... - emits - ESA
document title / titre du document TRP W ORK PLAN ... - emits - ESA
document title / titre du document TRP W ORK PLAN ... - emits - ESA
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<strong>TRP</strong> Work Plan 2005-2007<br />
Description of Activities<br />
TEC-SB/7935/dc<br />
12/Feb/09<br />
<strong>TRP</strong> Reference:<br />
Title:<br />
T603-03ES<br />
Robust LPV Gain Sche<strong>du</strong>ling Techniques for Space Applications<br />
Gain-sche<strong>du</strong>ling is perhaps one of the most popular approaches to non-linear control design and has been widely and<br />
successfully applied in fields ranging from aerospace to process control. The traditional control design proce<strong>du</strong>re consists of<br />
decomposing a non-linear time-varying problem into a number (operating conditions) of linear time invariant sub-problems. To<br />
verify that the closed-loop system behaves as expected and required between the operating conditions, extensive simulations<br />
and analysis are needed. A recent gain sche<strong>du</strong>ling method, so-called Linear Parameter Varying (LPV) technique, address the<br />
issue of system parametrisation and directly offer an optimal solution. As the intermediate step of linearization and stationary<br />
control design is suppressed, the design verification effort is drastically re<strong>du</strong>ced. The aim of the proposed activity is to<br />
evaluate, benchmark and demonstrate the benefits in validation effort of LPV gain sche<strong>du</strong>ling techniques when applied to the<br />
design of robust controllers for uncertain time-varying systems. In addition, robust LPV-based controller design proce<strong>du</strong>res<br />
and tool(s) that interface with in<strong>du</strong>strial requirements will be developed. The expected benefits is a drastic re<strong>du</strong>ction in control<br />
design verification effort for non-linear time-varying systems.<br />
Deliverables:<br />
Robust LPV gain-sche<strong>du</strong>led control design toolbox including benchmark models and <strong>document</strong>ation (technical data package,<br />
summary report and abstract).<br />
Current TRL:<br />
Target TRL: Beta Application Need/Date:<br />
-<br />
version<br />
Application/Mission: all missions Contract Duration: 24 months<br />
SW Clause : Open Source Code Dossier0 Ref.: T-7817<br />
Consistency with Harmonisation<br />
Roadmap: N/A<br />
Roadmap and Conclusions:<br />
<strong>TRP</strong> Reference: T603-04ES<br />
Title:<br />
Robust Model Predictive Control (MPC) for Space Constrained Systems<br />
Model Predictive Control (MPC) is a widely used and well accepted controller design method in the process in<strong>du</strong>stry. The<br />
most appealing feature of this type of control is its ability to cope with constrained systems. Robust formulation of MPC<br />
problems which take into account model uncertainties are also available, and are subject of intensive current research.<br />
Furthermore, MPC can be combined with other control techniques such as H2/Hinfinity. Finally, the dramatically increasing<br />
available computer power give new interest in such computer intensive techniques as they can easily take into account<br />
actuator limitations, non-linearities or non-stationarity. The aim of the proposed activity is to evaluate, benchmark and<br />
demonstrate the benefits of robust Model Predictive Control on critical space mission scenarios, such as time-bounded<br />
manoeuvres, saturated control and terminal guidance that are difficult to address with classical techniques. In addition,<br />
real-time performance (CPU, memory, etc.) will be assessed, and robust MPC design proce<strong>du</strong>res and tool(s) that interface<br />
with in<strong>du</strong>strial requirements will be developed.<br />
Deliverables:<br />
Robust MPC control design toolbox including benchmark models and <strong>document</strong>ation (technical data package, summary<br />
report, and abstract).<br />
Current TRL:<br />
Target TRL: Beta Application Need/Date:<br />
TRL1<br />
version<br />
Application/Mission: all missions Contract Duration: 24 months<br />
SW Clause : Operational SW Dossier0 Ref.: T-7817<br />
Consistency with Harmonisation<br />
Not directly linked to harmonised technology.<br />
Roadmap and Conclusions:<br />
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