The accuracy of the line-of-sight of aviation photoelectric optoelectronic stabilization platforms is limited by two factors: external disturbance and sensor noise. An extended state observer (ESO) can effectively improve their anti-interference ability. However, due to the serious problem of gyroscope noise, further improvement of an ESO’s disturbance suppression effect is limited. This article proposes a control structure that combines a Kalman filter (KF) and ESO, effectively improving upon the interference suppression ability of a traditional ESO under the influence of noise. Firstly, an ESO was used to observe the lumped disturbance of the system, and then, the observed disturbance was compensated for in the control loop. Secondly, bas...
This study designs a trigger to determine the number of layers of a multi-layer adaptive Kalman filt...
Abstract: The disturbances to an airframe’s sensors caused by the flexibility of the airframe is cal...
The presence of external disturbances such as wind may affect the stability of a quadrotor during fl...
A primary cause of degraded performance in pointing and tracking systems is the jitter in the line o...
In this paper the problem of detecting and isolating sensor faults on a general aviation aircraft, i...
The control of autonomous flying vehicles with navigation purposes is a challenging task. Complexity...
In unmanned systems an autopilot controls the outputs of the vehicle withouthuman interference. All ...
An extended signal-correction observer (ES-CO) is presented for signals correction and estimation, w...
The purpose of the research was to create an algorithm for determining and correcting the output par...
Aiming at the problem of mechanical resonance faced by the servo control system of the aero-optical ...
The main sources of noise and pick-ups in Alcator C-Mod are iden-tified and their effects on the mea...
ABSTRACT: The present article deals with the identification, at the same time, of aircraft stability...
The problem of detecting and isolating sensor faults (sensor fault detection and isolation—SFDI) on ...
An Extended Kalman Filter is designed in order to estimate both state variables and wind velocity ve...
ABSTRACT This paper discusses the synthesis of an Extended Kalman Filter (EKF) to perform both wind ...
This study designs a trigger to determine the number of layers of a multi-layer adaptive Kalman filt...
Abstract: The disturbances to an airframe’s sensors caused by the flexibility of the airframe is cal...
The presence of external disturbances such as wind may affect the stability of a quadrotor during fl...
A primary cause of degraded performance in pointing and tracking systems is the jitter in the line o...
In this paper the problem of detecting and isolating sensor faults on a general aviation aircraft, i...
The control of autonomous flying vehicles with navigation purposes is a challenging task. Complexity...
In unmanned systems an autopilot controls the outputs of the vehicle withouthuman interference. All ...
An extended signal-correction observer (ES-CO) is presented for signals correction and estimation, w...
The purpose of the research was to create an algorithm for determining and correcting the output par...
Aiming at the problem of mechanical resonance faced by the servo control system of the aero-optical ...
The main sources of noise and pick-ups in Alcator C-Mod are iden-tified and their effects on the mea...
ABSTRACT: The present article deals with the identification, at the same time, of aircraft stability...
The problem of detecting and isolating sensor faults (sensor fault detection and isolation—SFDI) on ...
An Extended Kalman Filter is designed in order to estimate both state variables and wind velocity ve...
ABSTRACT This paper discusses the synthesis of an Extended Kalman Filter (EKF) to perform both wind ...
This study designs a trigger to determine the number of layers of a multi-layer adaptive Kalman filt...
Abstract: The disturbances to an airframe’s sensors caused by the flexibility of the airframe is cal...
The presence of external disturbances such as wind may affect the stability of a quadrotor during fl...