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Found 11 papers, 2 papers with code
European Satellite Benchmark for Control Education and Industrial Training
To overcome the innovation gap of the Guidance, Navigation and Control (GNC) design process between research and industrial practice a benchmark of industrial relevance has been developed and is presented.
Launcher Attitude Control based on Incremental Nonlinear Dynamic Inversion: A Feasibility Study Towards Fast and Robust Design Approaches
The so-called ``New Space era'' has seen a disruptive change in the business models and manufacturing technologies of launch vehicle companies.
Robust Optimal Control for Nonlinear Systems with Parametric Uncertainties via System Level Synthesis
The proposed approach jointly optimizes a nominal nonlinear trajectory and an error feedback, requiring minimal offline design effort and offering low conservatism.
Asynchronous Computation of Tube-based Model Predictive Control
Tube-based model predictive control (MPC) methods bound deviations from a nominal trajectory due to uncertainties in order to ensure constraint satisfaction.
Reconfiguration of a satellite constellation in circular formation orbit with decentralized model predictive control
In this context, we consider the problem of reconfiguration of a satellite constellation in a circular formation.
Finite Horizon Worst-Case Analysis of Linear Time-Varying Systems Applied to Launch Vehicle
A condition for the worst-case gain of such an interconnection can be formulated using dissipation theory as a parameterized Riccati differential equation, which depends on the chosen IQC multiplier.
System Level Disturbance Reachable Sets and their Application to Tube-based MPC
Tube-based model predictive control (MPC) methods leverage tubes to bound deviations from a nominal trajectory due to uncertainties in order to ensure constraint satisfaction.
Optimal Science-time Reorientation Policy for the Comet Interceptor Flyby via Sequential Convex Programming
This paper introduces an algorithm to perform optimal reorientation of a spacecraft during a high speed flyby mission that maximizes the time a certain target is kept within the field of view of scientific instruments.
Autonomous parafoil precision landing using convex real-time optimized guidance and control
To overcome the limitations of current parafoil precision landing capabilities, an efficient real-time convex optimized guidance and control strategy is presented.
A System Level Approach to Tube-based Model Predictive Control
Robust tube-based model predictive control (MPC) methods address constraint satisfaction by leveraging an a priori determined tube controller in the prediction to tighten the constraints.
Multi-Objective Particle Swarm Optimization for Facility Location Problem in Wireless Mesh Networks
Wireless mesh networks have seen a real progress due of their implementation at a low cost.
