Advanced model-based FDIR techniques for aerospace systems: Today challenges and opportunities

A Zolghadri - Progress in Aerospace Sciences, 2012 - Elsevier
This paper discusses some trends and recent advances in model-based Fault Detection,
Isolation and Recovery (FDIR) for aerospace systems. The FDIR challenges range from pre …

[LIVRE][B] Fault diagnosis and fult-tolerant control and guidance for aerospace vehicles

A Zolghadri, D Henry, J Cieslak, D Efimov, P Goupil - 2014 - Springer
The impact that the aerospace and aviation industry has on today's modern society and
world's economy is very prominent. As such, the aerospace industry continues at the …

Global incremental flight control for agile maneuvering of a tailsitter flying wing

E Tal, S Karaman - Journal of Guidance, Control, and Dynamics, 2022 - arc.aiaa.org
This paper proposes a novel control law for accurate tracking of agile trajectories using a
tailsitter flying wing unmanned aerial vehicle that transitions between vertical takeoff and …

Robust adaptive backstep** control for reentry reusable launch vehicles

Z Wang, Z Wu, Y Du - Acta Astronautica, 2016 - Elsevier
During the reentry process of reusable launch vehicles (RLVs), the large range of flight
envelope will not only result in high nonlinearities, strong coupling and fast time-varying …

H ∞  ∕ H −  LPV solutions for fault detection of aircraft actuator faults: Bridging the gap between theory and practice

D Henry, J Cieslak, A Zolghadri… - International Journal of …, 2015 - Wiley Online Library
The work presented in this paper is undertaken within the European FP7 funded Advanced
Fault Diagnosis for Sustainable Flight Guidance and Control (ADDSAFE) project. The goal is …

Robust nonlinear stability and performance analysis of an F/A‐18 aircraft model using sum of squares programming

J Anderson, A Papachristodoulou - International Journal of …, 2013 - Wiley Online Library
In this paper, we develop algorithms for the computational analysis of stability and robust
performance properties of nonlinear models governed by polynomial differential equations …

[HTML][HTML] Commonalities between robust hybrid incremental nonlinear dynamic inversion and proportional-integral-derivative flight control law design

TSC Pollack, ST Theodoulis, E van Kampen - Aerospace Science and …, 2024 - Elsevier
Abstract Incremental Nonlinear Dynamic Inversion (INDI) has received substantial interest in
the recent years as a nonlinear flight control law design methodology that features inherent …

Transition flight control of two vertical/short takeoff and landing aircraft

Y **li, F Yong, Z Jihong - Journal of guidance, control, and dynamics, 2008 - arc.aiaa.org
THERE have been many types of vertical/short takeoff and landing (V/STOL) aircraft tested
over the past 50 years [1]. Notable V/STOL aircraft include the Harrier, powered by a …

Structured fault detection filters for LPV systems modeled in an LFR manner

D Henry - International Journal of Adaptive Control and Signal …, 2012 - Wiley Online Library
This paper investigates the design of robust‡ fault detection and isolation filters for linear
parameter‐varying systems modeled in a linear fractional representation fashion. The goal …

LPV modeling, analysis and design in space systems: Rationale, objectives and limitations

A Marcos, S Bennani - AIAA guidance, navigation, and control …, 2009 - arc.aiaa.org
Linear parameter varying theory has been in the control community for the last 15 years but
its use in space systems has been limited due to the slow transfer of these techniques to the …