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Asymmetric integral barrier Lyapunov function-based three-dimensional integrated guidance and control design with field-of-view constraint and input saturation

Advances in mechanical engineering, 2024-03, Vol.16 (3)

2024

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Fault-Tolerant Adaptive Asymptotic Attitude Tracking Control for a Rigid Spacecraft

Iranian journal of science and technology. Transactions of electrical engineering, 2021-12, Vol.45 (4), p.1383-1394

2021

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Field-of-View and Impact Angle Constrained Guidance Law for Missiles With Time-Varying Velocities

IEEE access, 2019, Vol.7, p.61717-61727

2019

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Generation of Guidance Commands for Civil Aircraft to Execute RNP AR Approach Procedure at High Plateau

Aerospace, 2023-04, Vol.10 (5), p.396

2023

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Nonlinear mapping based impact angle control guidance with seeker's field-of-view constraint

Aerospace science and technology, 2019-03, Vol.86, p.724-736

2019

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Predefined-Time Asymptotic Tracking Control for Hypersonic Flight Vehicles With Input Quantization and Faults

IEEE transactions on aerospace and electronic systems, 2021-10, Vol.57 (5), p.2826-2837

2021

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Asymptotic tracking control for uncertain strict‐feedback nonlinear systems with delayed full‐state constraints

International journal of robust and nonlinear control, 2020-12, Vol.30 (18), p.8174-8191

2020

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Continuous precise predefined-time attitude tracking control for a rigid spacecraft

International journal of control, 2023-04, Vol.96 (4), p.922-934

2023

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Cooperative task allocation for multi heterogeneous aerial vehicles using particle swarm optimization algorithm and entropy weight method

Applied soft computing, 2023-11, Vol.148, p.110918, Article 110918

2023

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Asymmetric integral barrier Lyapunov function-based adaptive tracking control considering full-state with input magnitude and rate constraint

Journal of the Franklin Institute, 2020-09, Vol.357 (14), p.9709-9732

2020

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Three-dimensional impact angle control guidance with field-of-view constraint

Aerospace science and technology, 2020-10, Vol.105, p.106014, Article 106014

2020

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Adaptive Attitude Stabilization Control Design for Spacecraft Under Physical Limitations

Journal of guidance, control, and dynamics, 2016-09, Vol.39 (9), p.2179-2183

2016

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Predefined‐time backstepping control for a nonlinear strict‐feedback system

International journal of robust and nonlinear control, 2021-05, Vol.31 (8), p.3354-3372

2021

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Angle-of-attack and angle-of-sideslip estimation and complementary filter design for civil aircraft

ISA transactions, 2024-08

2024

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Predefined-time adaptive fault-tolerant control of hypersonic flight vehicles without overparameterization

Aerospace science and technology, 2020-09, Vol.104, p.105987, Article 105987

2020

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A novel estimation method for weight and center-of-gravity via the aircraft trim data

Measurement : journal of the International Measurement Confederation, 2023-10, Vol.220, p.113362, Article 113362

2023

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Predefined‐time control for Euler–Lagrange systems with model uncertainties and actuator faults

Asian journal of control, 2023-03, Vol.25 (2), p.1591-1605

2023

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Midcourse trajectory optimization strategy for air-to-air missile based on Gauss Pseudo-spectral Method

Proceedings of the 32nd Chinese Control Conference, 2013, p.4889-4893

2013

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Optimal low-thrust trajectory design and robust tracking control for spacecraft rendezvous

Proceedings of the 32nd Chinese Control Conference, 2013, p.4885-4888

2013

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Fixed-time Integrated Guidance and Control with Impact Angle Constraint

2022 41st Chinese Control Conference (CCC), 2022, p.3317-3322

2022

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Evaluation and selection of missile's optimal initial launch azimuth under side window detection using a hybrid decision making method

Aerospace science and technology, 2018-05, Vol.76, p.217-228

2018

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MicroRNA‐135a alleviates oxygen‐glucose deprivation and reoxygenation‐induced injury in neurons through regulation of GSK‐3β/Nrf2 signaling

Journal of biochemical and molecular toxicology, 2018-07, Vol.32 (7), p.e22159-n/a

2018

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Constrained dual-loop attitude control design for spacecraft

Aerospace science and technology, 2016-08, Vol.55, p.170-176

2016

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SEPT7 overexpression inhibits glioma cell migration by targeting the actin cytoskeleton pathway

Oncology reports, 2016-04, Vol.35 (4), p.2003-2010

2016

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Predefined-Time Attitude Tracking Control of a Rigid Spacecraft

2021 40th Chinese Control Conference (CCC), 2021, p.427-432

2021

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Asymmetric integral barrier Lyapunov function-based three-dimensional integrated guidance and control design with field-of-view constraint and input saturation

Fault-Tolerant Adaptive Asymptotic Attitude Tracking Control for a Rigid Spacecraft

Field-of-View and Impact Angle Constrained Guidance Law for Missiles With Time-Varying Velocities

Generation of Guidance Commands for Civil Aircraft to Execute RNP AR Approach Procedure at High Plateau

Nonlinear mapping based impact angle control guidance with seeker's field-of-view constraint

Predefined-Time Asymptotic Tracking Control for Hypersonic Flight Vehicles With Input Quantization and Faults

Asymptotic tracking control for uncertain strict‐feedback nonlinear systems with delayed full‐state constraints

Continuous precise predefined-time attitude tracking control for a rigid spacecraft

Cooperative task allocation for multi heterogeneous aerial vehicles using particle swarm optimization algorithm and entropy weight method

Asymmetric integral barrier Lyapunov function-based adaptive tracking control considering full-state with input magnitude and rate constraint

Three-dimensional impact angle control guidance with field-of-view constraint

Adaptive Attitude Stabilization Control Design for Spacecraft Under Physical Limitations

Predefined‐time backstepping control for a nonlinear strict‐feedback system

Angle-of-attack and angle-of-sideslip estimation and complementary filter design for civil aircraft

Predefined-time adaptive fault-tolerant control of hypersonic flight vehicles without overparameterization

A novel estimation method for weight and center-of-gravity via the aircraft trim data

Predefined‐time control for Euler–Lagrange systems with model uncertainties and actuator faults

Midcourse trajectory optimization strategy for air-to-air missile based on Gauss Pseudo-spectral Method

Optimal low-thrust trajectory design and robust tracking control for spacecraft rendezvous

Fixed-time Integrated Guidance and Control with Impact Angle Constraint

Evaluation and selection of missile's optimal initial launch azimuth under side window detection using a hybrid decision making method

MicroRNA‐135a alleviates oxygen‐glucose deprivation and reoxygenation‐induced injury in neurons through regulation of GSK‐3β/Nrf2 signaling

Constrained dual-loop attitude control design for spacecraft

SEPT7 overexpression inhibits glioma cell migration by targeting the actin cytoskeleton pathway

Predefined-Time Attitude Tracking Control of a Rigid Spacecraft

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