Based on both adaptive and fuzzy logic techniques, the fault-tolerant tracking problem for near-space vehicle (NSV) with actuator faults is investigated in this paper. First, the nonlinear NSV attitude dynamics is given, which can represent the dynamic characteristics of NSV in both ascent and re-entry phases. The actuator fault under consideration in this study is the loss of effectiveness, and a novel fault detection scheme is presented by designing a nonlinear fault detection observer. In terms of fault detection information and multi-observer technique, a fault isolation scheme is proposed. Taking advantage of a fuzzy logic system (FLS) to approximate the unknown nonlinear function, an adaptive FLS-based fault-tolerant tracking control ...
The problem of finite-time attitude-tracking control (ATC) for a rigid spacecraft subject to inertia...
In this paper, the problem of active fault tolerant control for a reusable launch vehicle (RLV) with...
This paper presents a novel fault diagnosis method for satellite attitude control systems. Under Lip...
Based on the adaptive-control technique, this paper deals with the problem of fault-tolerant trackin...
Based on the adaptive-control technique, this paper dealswith the problem of fault-tolerant trackin...
Based on both adaptive and fuzzy control techniques, this paper proposes a fault-tolerant control (F...
Based on both adaptive and sliding mode control techniques, this paper pro-\ud poses an integrated a...
Based on both adaptive and sliding mode control techniques, this paper pro- poses an integrated app...
In this paper, a decentralized fault-tolerant control (FTC) system is proposed for near-space vehicl...
In this paper, a novel adaptive dynamic sliding mode (ADSM) fault-tolerant control (FTC) methodology...
An adaptive fuzzy fault-tolerant tracking controller is developed for Near-Space Vehicles (NSVs) suf...
In this paper, an adaptive sliding mode (ASM) scheme is proposed for fault identification and fault-...
In this paper, a fault-tolerant control scheme based on a second-order dynamic terminal sliding mode...
This paper develops a fault-tolerant attitude controller for next-generation nanosatellites. The pro...
In this study, a theoretical framework for reconfigurable flight control is developed and applied to...
The problem of finite-time attitude-tracking control (ATC) for a rigid spacecraft subject to inertia...
In this paper, the problem of active fault tolerant control for a reusable launch vehicle (RLV) with...
This paper presents a novel fault diagnosis method for satellite attitude control systems. Under Lip...
Based on the adaptive-control technique, this paper deals with the problem of fault-tolerant trackin...
Based on the adaptive-control technique, this paper dealswith the problem of fault-tolerant trackin...
Based on both adaptive and fuzzy control techniques, this paper proposes a fault-tolerant control (F...
Based on both adaptive and sliding mode control techniques, this paper pro-\ud poses an integrated a...
Based on both adaptive and sliding mode control techniques, this paper pro- poses an integrated app...
In this paper, a decentralized fault-tolerant control (FTC) system is proposed for near-space vehicl...
In this paper, a novel adaptive dynamic sliding mode (ADSM) fault-tolerant control (FTC) methodology...
An adaptive fuzzy fault-tolerant tracking controller is developed for Near-Space Vehicles (NSVs) suf...
In this paper, an adaptive sliding mode (ASM) scheme is proposed for fault identification and fault-...
In this paper, a fault-tolerant control scheme based on a second-order dynamic terminal sliding mode...
This paper develops a fault-tolerant attitude controller for next-generation nanosatellites. The pro...
In this study, a theoretical framework for reconfigurable flight control is developed and applied to...
The problem of finite-time attitude-tracking control (ATC) for a rigid spacecraft subject to inertia...
In this paper, the problem of active fault tolerant control for a reusable launch vehicle (RLV) with...
This paper presents a novel fault diagnosis method for satellite attitude control systems. Under Lip...