Fault-tolerant control with mixed aerodynamic surfaces and RCS jets for hypersonic reentry vehicles

He, Jiping; Qi, Ruiyun; Jiang, Bin; Zhai, Rongyu

doi:10.1016/j.cja.2017.01.003

Cited by 32 publications

(24 citation statements)

References 36 publications

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“…Theorem 1. The terminal sliding mode surface S can converge to an expected region and thenq is uniformly ultimately bounded under the adaptive law expressed in equation (22). Proof 1.…”

Section: Outer Loop Terminal Sliding Mode Controllermentioning

confidence: 94%

Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm

Wang

Gong

Chen

2020

International Journal of Advanced Robotic Systems

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This study proposes a fault estimation and compensation scheme for hypersonic flight vehicle (HFV) attitude system with body flap fault. To achieve the fault compensation capability, an interval type-2 fuzzy estimator is designed to approximate the unknown nonlinear function caused by modeling uncertainties and the fault. The fault-tolerant controller via the terminal sliding mode and dynamic surface techniques is developed to ensure the tracking accuracy of attitude angles for HFV and the desired control torque can be achieved. Then, a novel control allocation scheme with a cuckoo search algorithm and linear programming method is proposed to distribute the desired torque to aerodynamic surfaces and reaction control system jets. The stability of the proposed scheme is analyzed using the Lyapunov stability theory. The validity of the method is verified by a series of comparisons on numerical simulation results.

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“…Theorem 1. The terminal sliding mode surface S can converge to an expected region and thenq is uniformly ultimately bounded under the adaptive law expressed in equation (22). Proof 1.…”

Section: Outer Loop Terminal Sliding Mode Controllermentioning

confidence: 94%

Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm

Wang

Gong

Chen

2020

International Journal of Advanced Robotic Systems

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“…Consequently, RCS is a better solution scheme to provide efficient control performance. Currently, a lot of research studies on RCS are focused on RCS thruster configuration [2], RCS nozzle selection logic [3,4], and RCS combined with pneumatic rudder surface control [5,6]. Liu provides a new method to obtain necessary and sufficient conditions for impulse controllability in continuous linear dynamics, which performs discrete-time actions for spacecraft maneuvering [7].…”

Section: Introductionmentioning

confidence: 99%

Reaction Control System Optimization for Maneuverable Reentry Vehicles Based on Particle Swarm Optimization

Gui

Sun

Chen

et al. 2020

Discrete Dynamics in Nature and Society

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This paper presents a new parametric optimization design to solve a class of reaction control system (RCS) problem with discrete switching state, flexible working time, and finite-energy control for maneuverable reentry vehicles. Based on basic particle swarm optimization (PSO) method, an exponentially decreasing inertia weight function is introduced to improve convergence performance of the PSO algorithm. Considering the PSO algorithm spends long calculation time, a suboptimal control and guidance scheme is developed for online practical design. By tuning the control parameters, we try to acquire efficacy as close as possible to that of the PSO-based solution which provides a reference. Finally, comparative simulations are conducted to verify the proposed optimization approach. The results indicate that the proposed optimization and control algorithm has good performance for such RCS of maneuverable reentry vehicles.

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“…[1][2][3][4][5][6][7][8] To realize these attitude control methods, attention should be paid to the attitude control effectors. Control effectors of reentry vehicles generally consist of aerodynamic surfaces, 2,[4][5][6] moving mass, [8][9][10][11] and reaction control system (RCS). 2,4,6,7 Aerodynamic surfaces are the mainstream attitude actuators of reentry vehicles.…”

Section: Introductionmentioning

confidence: 99%

“…Control effectors of reentry vehicles generally consist of aerodynamic surfaces, 2,[4][5][6] moving mass, [8][9][10][11] and reaction control system (RCS). 2,4,6,7 Aerodynamic surfaces are the mainstream attitude actuators of reentry vehicles. However, the aerodynamic heating during the reentry process may be too high to make the aerodynamic surfaces ineffective.…”

Section: Introductionmentioning

confidence: 99%

“…RCS is usually adopted as an auxiliary actuator, especially used to provide control torque at high altitudes where the primary actuators are unable to efficiently work. 4 However, attitude control using RCS cannot guarantee high accuracy due to the delay property of the RCS jets. 13 To overcome the above drawbacks of the current actuators, some researchers have attempted to adopt the attitude actuators used in the spacecraft to substitute for the currently used ones.…”

Section: Introductionmentioning

confidence: 99%

See 1 more Smart Citation

Attitude control of reentry vehicles in roll channel using single-gimbal control moment gyros and a reaction control system

Liu

2017

Advances in Mechanical Engineering

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A novel roll-channel attitude control scheme using a combination of single-gimbal control moment gyros and a reaction control system is proposed, providing sufficient control torque during the whole reentry process. A scissored-pair configuration is applied to the single-gimbal control moment gyros, which guarantees control torque exclusively along the roll axis and avoids internal singularity. A sliding-mode attitude controller is proposed to meet the requirements of rollchannel attitude stability and disturbance rejection. To obtain an optimal allocation of the commanded torque to the single-gimbal control moment gyros and the reaction control system, an allocation method based on fuzzy reasoning is proposed. To render the design and validation of the control scheme close to reality, the responsiveness of the singlegimbal control moment gyro is considered, and the discrete and delay properties of the reaction control system are included. The steering logic of the single-gimbal control moment gyro and the modulator of the reaction control system are designed, respectively. Numerical simulation is performed to verify the proposed control scheme. Moreover, a hardware-in-the-loop simulation system based on an air-bearing test bed is developed to conduct experiments for convincingly validating the proposed attitude control method. The feasibility and good performance of the proposed control scheme are verified by the results of the numerical simulation and the experiment.

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Fault-tolerant control with mixed aerodynamic surfaces and RCS jets for hypersonic reentry vehicles

Cited by 32 publications

References 36 publications

Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm

Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm

Reaction Control System Optimization for Maneuverable Reentry Vehicles Based on Particle Swarm Optimization

Attitude control of reentry vehicles in roll channel using single-gimbal control moment gyros and a reaction control system

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