Contact

Jiannan Zhang
M. Sc.
E-mail:jiannan.zhang@tum.de

Publications

[12] J. Zhang, M. Söpper and F. Holzapfel, "Attainable Moment Set Optimization to Support Configuration Design: A Required Moment Set Based Approach", MDPI Applied Sciences, vol. 11, no. 8, 2021.
[11] J. Zhang, F. Holzapfel, "Saturation Protection with Pseudo Control Hedging: A Control Allocation Perspective", in AIAA SciTech 2021 Forum. [doi]
[10] M. Söpper, J. Zhang, N. Bähr, F. Holzapfel, "Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models", MDPI Applied Sciences, vol. 11, no. 8, 2021. [doi]
[9] J. Zhang, J. Wang, F. Zhang, F. Holzapfel, "Modeling and Incremental Nonlinear Dynamic Inversion Control for a Highly Redundant Flight System​", in AIAA Scitech 2019 Forum. [doi]
[8] J. Zhang, P. Bhardwaj, S. Raab, F. Holzapfel, "Control Allocation Framework with SVD-based Protection for a Tilt-rotor VTOL Transition Air Vehicle", in AIAA Aviation 2019 Forum. [doi]
[7] S. Raab, J. Zhang, P. Bhardwaj, F. Holzapfel, "Consideration of Control Effector Dynamics and Saturations in an Extended INDI Approach", in AIAA Aviation 2019 Forum. [doi]
[6] P. Bhardwaj, V. S. Akkinapalli, J. Zhang, S. Saboo, F. Holzapfel, "Adaptive Augmentation of Incremental Nonlinear Dynamic Inversion Controller for an Extended F-16 Model", in AIAA Scitech 2019 Forum.
[5] P. Bhardwaj, S. Raab, J. Zhang, F. Holzapfel, "​​​Thrust command based Integrated Reference Model with Envelope Protections for Tilt-rotor VTOL Transition UAV", in AIAA Aviation 2019 Forum. [doi]
[4] J. Zhang, P. Bhardwaj, S. Raab, S. Saboo, F. Holzapfel, "Control Allocation Framework for a Tilt-rotor Vertical Take-off and Landing Transition Aircraft Configuration", in 2018 AIAA Applied Aerodynamics Conference. [doi]
[3] S. Raab, J. Zhang, P. Bhardwaj, F. Holzapfel, "Proposal of a Unified Control Strategy for Vertical Take-off and Landing Transition Aircraft Configurations​", in 2018 AIAA Applied Aerodynamics Conference. [doi]
[2] P. Bhardwaj, S. Raab, J. Zhang, F. Holzapfel, "Integrated Reference Model for a Tilt-rotor Vertical Takeoff and Landing Transition UAV", in AIAA AVIATION 2018. [doi]
[1] J. Diepolder, S. Saboo, V. S. Akkinapalli, S. Raab, J. Zhang, P. Bhardwaj, M. Krenmayr, B. Grüter, F. Holzapfel, "Flight Control Law Testing using Optimal Control and Postoptimal Sensitivity Analysis", in CEAS EuroGNC, 2017.

Supervised Student Theses

[6] C. Mühlbach, "Development of a Framework of Attainable Moment Set Optimization for eVTOLs​", Thesis, Technische Universität München, Garching, 2021.
[5] S. Ma, "Control Set Based Configuration Optimization of a Distributed Electric Propulsion Aircraft​", Thesis, Technische Universität München, Garching, 2021.
[4] Y. Li, "Implementation and Verification of a Standard Control Allocation Library​", Thesis, Technische Universität München, Garching, 2021.
[3] N. Michel, "Incremental Nonlinear Dynamic Inversion of the Longitudinal Dynamics of a Transition Vehicle Including Nonlinear Coupling Effects​", Thesis, Technische Universität München, Garching, 2019.
[2] S. Saboo, "Control Allocation Approaches with application to extended F-16 model and tilt-rotor UAV", Thesis, Technische Universität München, Garching, 2017.
[1] M. Meissner, "Onboard Plant Model for Incremental Nonlinear Controller Structures", Thesis, Technische Universität München, Garching, 2017.