TA
T. Aantjes
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2 records found
1
Master thesis
(2025)
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T. Aantjes, E.J.J. Smeur, Spilios Theodoulis, T.M. Blaha, S. Hamaza, A. Bombelli
This work presents the design of a robust gain-scheduled controller for attitude control of quadcopters, using an Incremental Nonlinear Dynamic Inversion (INDI)-based inner loop with online identification of its system parameters. A linearized model including uncertainty in the identified parameters and unmodeled dynamics is presented for robustness analysis, followed by a set of design requirements. With this, a cascaded feedback attitude controller with a feedforward filter was synthesized for a symmetric quadcopter using signal-based H-infinity closed-loop shaping. Subsequent linear analysis demonstrated good robustness margins and performance characteristics, which were further validated through nonlinear simulations and experimental flights, showing good performance under uncertainty.
This methodology was then extended using co-design to develop a gain-schedule for varying actuator time constants. The approach achieved the requirements over the entire range. The resulting gain-scheduled controller exhibited good stability margins, with nonlinear simulations confirming effective tracking performance under uncertainty. Experimental evaluation of the gain-scheduled controller was conducted through flight tests with full online parameter identification. Even though the identified parameters during these tests were far outside the defined uncertainty range, acceptable flight performance comparable to simulation results was maintained for actuator time constants below 40 ms. For slower actuators, performance was degraded but this may have been due to the extreme uncertainties rather than the controller itself. ...
This methodology was then extended using co-design to develop a gain-schedule for varying actuator time constants. The approach achieved the requirements over the entire range. The resulting gain-scheduled controller exhibited good stability margins, with nonlinear simulations confirming effective tracking performance under uncertainty. Experimental evaluation of the gain-scheduled controller was conducted through flight tests with full online parameter identification. Even though the identified parameters during these tests were far outside the defined uncertainty range, acceptable flight performance comparable to simulation results was maintained for actuator time constants below 40 ms. For slower actuators, performance was degraded but this may have been due to the extreme uncertainties rather than the controller itself. ...
This work presents the design of a robust gain-scheduled controller for attitude control of quadcopters, using an Incremental Nonlinear Dynamic Inversion (INDI)-based inner loop with online identification of its system parameters. A linearized model including uncertainty in the identified parameters and unmodeled dynamics is presented for robustness analysis, followed by a set of design requirements. With this, a cascaded feedback attitude controller with a feedforward filter was synthesized for a symmetric quadcopter using signal-based H-infinity closed-loop shaping. Subsequent linear analysis demonstrated good robustness margins and performance characteristics, which were further validated through nonlinear simulations and experimental flights, showing good performance under uncertainty.
This methodology was then extended using co-design to develop a gain-schedule for varying actuator time constants. The approach achieved the requirements over the entire range. The resulting gain-scheduled controller exhibited good stability margins, with nonlinear simulations confirming effective tracking performance under uncertainty. Experimental evaluation of the gain-scheduled controller was conducted through flight tests with full online parameter identification. Even though the identified parameters during these tests were far outside the defined uncertainty range, acceptable flight performance comparable to simulation results was maintained for actuator time constants below 40 ms. For slower actuators, performance was degraded but this may have been due to the extreme uncertainties rather than the controller itself.
This methodology was then extended using co-design to develop a gain-schedule for varying actuator time constants. The approach achieved the requirements over the entire range. The resulting gain-scheduled controller exhibited good stability margins, with nonlinear simulations confirming effective tracking performance under uncertainty. Experimental evaluation of the gain-scheduled controller was conducted through flight tests with full online parameter identification. Even though the identified parameters during these tests were far outside the defined uncertainty range, acceptable flight performance comparable to simulation results was maintained for actuator time constants below 40 ms. For slower actuators, performance was degraded but this may have been due to the extreme uncertainties rather than the controller itself.
Bachelor thesis
(2022)
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A. Singh, A.P. Tripathi, T. Aantjes, S. Blaga, A. Pavlov, V. Gupta, G. Basile, D.F. Bolkestein, M.L. Mazurkiewicz, I.A. Quintanilla Rojas, I. Uriol Balbin, C.J. van Calcar, Y. Wu, Stijn Mast
Maintaining a high speed, secure and robust connection to the world is of paramount importance
in modern society. This proved especially true during a recent volcanic eruption in the small island nation of Tonga, where the only optical fibre line to the country was severed due to the cataclysm, completely disconnecting the island from the rest of the world. The lack of communication made the disaster relief to the eruption more complex. The Emergency Communications Node (ECN) can be deployed within 48 hours to enable alternative means of communication that replace damaged communication lines... ...
in modern society. This proved especially true during a recent volcanic eruption in the small island nation of Tonga, where the only optical fibre line to the country was severed due to the cataclysm, completely disconnecting the island from the rest of the world. The lack of communication made the disaster relief to the eruption more complex. The Emergency Communications Node (ECN) can be deployed within 48 hours to enable alternative means of communication that replace damaged communication lines... ...
Maintaining a high speed, secure and robust connection to the world is of paramount importance
in modern society. This proved especially true during a recent volcanic eruption in the small island nation of Tonga, where the only optical fibre line to the country was severed due to the cataclysm, completely disconnecting the island from the rest of the world. The lack of communication made the disaster relief to the eruption more complex. The Emergency Communications Node (ECN) can be deployed within 48 hours to enable alternative means of communication that replace damaged communication lines...
in modern society. This proved especially true during a recent volcanic eruption in the small island nation of Tonga, where the only optical fibre line to the country was severed due to the cataclysm, completely disconnecting the island from the rest of the world. The lack of communication made the disaster relief to the eruption more complex. The Emergency Communications Node (ECN) can be deployed within 48 hours to enable alternative means of communication that replace damaged communication lines...