Robust autopilot design for landing a large civil aircraft in crosswind

J Theis, D Ossmann, F Thielecke, H Pfifer - Control Engineering Practice, 2018 - Elsevier
A comprehensive autolanding design for a representative model of a twin-engined
commercial aircraft is presented in this paper. To facilitate the design task and minimize …

Flight testing automatic landing control for unmanned aircraft including curved approaches

N Sedlmair, J Theis, F Thielecke - Journal of guidance, control, and …, 2022 - arc.aiaa.org
Automatic landing of aircraft is a challenging guidance and control task that requires multiple
feedback loops and a precise sequence of actions. Increasing operational flexibility and …

Application of structured robust synthesis for flexible aircraft flutter suppression

B Patartics, G Lipták, T Luspay, P Seiler… - … on Control Systems …, 2021 - ieeexplore.ieee.org
This article presents a method for structured robust control design for systems with a mixture
of parametric and dynamic uncertainty. The proposed method alternates between an …

Robust tuning of geometric attitude controllers for multirotor unmanned aerial vehicles

D Invernizzi, S Panza, M Lovera - Journal of Guidance, Control, and …, 2020 - arc.aiaa.org
In recent years there has been a significant body of literature proposing nonlinear attitude
control laws for small-scale multirotor unmanned aerial vehicles (UAVs), motivated by the …

Automatic take-off and landing of tailwheel aircraft with incremental nonlinear dynamic inversion

A Steinleitner, V Frenzel, O Pfeifle, J Denzel… - AIAA Scitech 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1228. vid This work presents a
control and guidance algorithm for automated tailwheel aircraft operation during takeoff and …

SAR optimization and Convolutional Neural Network based fault estimations and for auto-landing control model

T Ayyasamy, S Nirmala, A Saravanakumar - Robotics and Autonomous …, 2023 - Elsevier
During auto landing, the aircraft flies at a significantly low altitude and low speed. So the
consequent accidents and flight crashes are highly possible. Several constrained space and …

LFT modeling and μ analysis of the aircraft landing benchmark

A Iannelli, P Simplício, D Navarro-Tapia, A Marcos - IFAC-PapersOnLine, 2017 - Elsevier
The landing of a civil transport aircraft is one of the most challenging phases. The reason
mainly lies in the need to satisfy different concurrent requirements in the face of a wide …

Combining Stable Inversion and H Synthesis for Trajectory Tracking and Disturbance Rejection Control of Civil Aircraft Autolanding

X Wang, Y Sang, G Zhou - Applied Sciences, 2020 - mdpi.com
The landing phase during a flight probably is the most dangerous part, as most of the
accidents occur in this phase. A robust trajectory tracking controller is presented to autoland …

The usability analysis of software loading tools in a commercial airline

AA Abella, YT Prasetyo, MML Cahigas, RB Dela Cruz… - Work, 2024 - content.iospress.com
Background: Aircraft software loading tools evolved as enhanced floppy disks and different
types of portable data loaders emerged into the modern world. However, there was a lack of …

Robust autoland design by multi-model H∞ synthesis with a focus on the flare phase

JM Biannic, C Roos - Aerospace, 2018 - mdpi.com
Recent advances in the resolution of multi-model and multi-objective control problems via
non-smooth optimization are exploited to provide a novel methodology in the challenging …