Sensitivity of piezoresistive pressure sensors to acceleration
Z Szczerba, P Szczerba, K Szczerba - Energies, 2022 - mdpi.com
The article presents the negative aspects of the influence of static and dynamic acceleration
on the accuracy of pressure measurement for a selected type of transmitter. The influence of …
on the accuracy of pressure measurement for a selected type of transmitter. The influence of …
Fixed wing aircraft automatic landing with the use of a dedicated ground sign system
B Brukarczyk, D Nowak, P Kot, T Rogalski, P Rzucidło - Aerospace, 2021 - mdpi.com
The paper presents automatic control of an aircraft in the longitudinal channel during
automatic landing. There are two crucial components of the system presented in the paper: a …
automatic landing. There are two crucial components of the system presented in the paper: a …
The papi lights-based vision system for aircraft automatic control during approach and landing
The paper presents the concept of a component of an aircraft's automatic flight control
system, controlling the airplane when in longitudinal motion (ie, pitch angle, sink rate …
system, controlling the airplane when in longitudinal motion (ie, pitch angle, sink rate …
Acceleration-Insensitive Pressure Sensor for Aerodynamic Analysis
Z Szczerba, P Szczerba, K Szczerba, K Pytel - Energies, 2023 - mdpi.com
This paper presents a method for preparing a pressure sensor that is insensitive to
acceleration along with experimental evidence of its efficacy in aerodynamic analysis. A …
acceleration along with experimental evidence of its efficacy in aerodynamic analysis. A …
The use of vision system to determine lateral deviation from landing trajectory
T Rogalski, P Rzucidło, S Noga… - Aircraft engineering and …, 2023 - emerald.com
Purpose This study presents an image processing algorithm capable of calculating selected
flight parameters requested by flight control systems to guide aircraft along the horizontal …
flight parameters requested by flight control systems to guide aircraft along the horizontal …
[PDF][PDF] Analysis of an aircraft departure and spin characteristics using Nash equilibrium theory
C Yan, L Tu, Y Yang, Y Wang - Journal of Theoretical and Applied …, 2023 - jtam.pl
The departure characteristics and steady-spin characteristics of a training aircraft are
analyzed. The sideslip departure characteristics of the aircraft under the maximum weight …
analyzed. The sideslip departure characteristics of the aircraft under the maximum weight …
[PDF][PDF] Acceleration-Insensitive Pressure Sensor for Aerodynamic Analysis. Energies 2023, 16, 3040
Z Szczerba, P Szczerba, K Szczerba, K Pytel - 2023 - academia.edu
This paper presents a method for preparing a pressure sensor that is insensitive to
acceleration along with experimental evidence of its efficacy in aerodynamic analysis. A …
acceleration along with experimental evidence of its efficacy in aerodynamic analysis. A …