Gain scheduling with guardian maps for longitudinal flight control
AMONG nonlinear control methods, gain scheduling is one of the most popular [1, 2], and
efforts have been made recently to put forth a unified framework for it [3]. There are mainly …
efforts have been made recently to put forth a unified framework for it [3]. There are mainly …
Switching control of a hypersonic vehicle based on guardian maps
D Xiao, M Liu, Y Liu, Y Lu - Acta Astronautica, 2016 - Elsevier
For the air-breathing hypersonic vehicles (AHSV) with a broad flight envelope, this paper
proposes a new controller design method to ensure robust stability in the presence of …
proposes a new controller design method to ensure robust stability in the presence of …
Stabilisation, tracking and disturbance rejection control design for the UAS-S45 Bálaam
The stabilisation and control mechanisms of an Unmanned Aerial System (UAS) must be
properly designed to ensure acceptable flight performance. During their operation, these …
properly designed to ensure acceptable flight performance. During their operation, these …
An efficient kriging modeling method based on multidimensional scaling for high-dimensional problems
Y Ge, J Shi, Y Li, J Shen - Algorithms, 2021 - mdpi.com
Kriging-based modeling has been widely used in computationally intensive simulations.
However, the Kriging modeling of high-dimensional problems not only takes more time, but …
However, the Kriging modeling of high-dimensional problems not only takes more time, but …
On the handling qualities of two flying wing aircraft configurations
LMBC Campos, JMG Marques - Aerospace, 2021 - mdpi.com
The coupling of the longitudinal and lateral stability modes of an aeroplane is considered in
two cases:(i) weak coupling, when the changes in the frequency and damping of the …
two cases:(i) weak coupling, when the changes in the frequency and damping of the …
Velocity‐Adaptive Prescribed Performance Control for Carrier‐Based Aircraft Based on Guardian Maps
C Li, J Lai, B Chen, Y Liu - International Journal of Aerospace …, 2023 - Wiley Online Library
The automatic carrier landing process is a significant and complex due to the plant variation
of carrier‐based aircraft. To reasonably identify the stability interval for specific performance …
of carrier‐based aircraft. To reasonably identify the stability interval for specific performance …
Wind Shear Response of Aircraft with C* and C* U Controller during Approach
Y Yan, L Song - Aerospace, 2024 - mdpi.com
This study investigates the impact of wind shear on the flight dynamics of commercial aircraft
where C* and C* U control laws are employed during the approach phase. Given the high …
where C* and C* U control laws are employed during the approach phase. Given the high …
Robust control of a launch vehicle in atmospheric ascent based on guardian maps
V Dubanchet, D Saussié, C Bérard… - 2012 American …, 2012 - ieeexplore.ieee.org
A robust control design for a space launcher during its atmospheric ascent is presented.
Considering a typical wind profile during flight, the launcher controller has to first stabilize …
Considering a typical wind profile during flight, the launcher controller has to first stabilize …
Aircraft pitch rate control design with guardian maps
A fixed architecture flight controller guaranteeing a priori given handling quality
requirements is proposed. Handling qualities are translated into pole confinement within a …
requirements is proposed. Handling qualities are translated into pole confinement within a …
Longitudinal stability and control augmentation with robustness and handling qualities requirements using the two degree of freedom controller
FJT Vargas, FJ de Oliveira Moreira… - Journal of the brazilian …, 2016 - Springer
This paper presents a practical design of longitudinal stability and control augmentation
system (SCAS) using a two degree of freedom (TDOF) controller. It is based on the linear …
system (SCAS) using a two degree of freedom (TDOF) controller. It is based on the linear …