This is the public page of the Optimization for Flight Control group (formerly known as ACSO) at the Institute of Flight Mechanics and Controls (iFR) of the University of Stuttgart. The group is dedicated to the analysis of complex aerospace control systems by means of nonlinear systems theory and optimization, the development of algorithms for optimization-based approaches, and optimal control of nonlinear systems.
iFR Optimization for Flight Control Group
Research group at the Institute of Flight Mechanics and Controls, University of Stuttgart
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TAC25-Inf-MPC
TAC25-Inf-MPC PublicSupplementary to: Safe-by-Design Approximate Nonlinear Model Predictive Control with Realtime Feasibility
C 1
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GTM_DesignSim
GTM_DesignSim PublicForked from nasa/GTM_DesignSim
NASA's Generic Transport Model
MATLAB
Repositories
Showing 9 of 9 repositories
- TAC25-Inf-MPC Public
Supplementary to: Safe-by-Design Approximate Nonlinear Model Predictive Control with Realtime Feasibility
- worst-case-probability-SOS Public
- ISS-Infinitesimal-MPC Public
This repository contains source code for the numerical result section in "Input-to-state Stable Nonlinear Model Predictive Control with Realtime Feasibility".
- SOS-Verify-Manifold-Spacecraft Public
Supplementary to: Sum of Squares Stability Verification on Manifolds with Applications in Spacecraft Attitude Control
- Sequential-SOS-Nonlinear-Control Public
This repository supplements the paper "Sequential Quadratic Sum-of-squares Programming for Nonlinear Control Systems" submitted to IEEE Transactions on Control Systems Technology. It contains the case studies for different analysis and control problems.
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- W23_RTGrundlagen_demo Public archive
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