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RLV integrated guidance and control based on adaptive high-order sliding mode
In this paper, a novel integrated guidance and control algorithm based on adaptive high-order sliding mode is proposed for reusable launch vehicle...
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Integrated Guidance and Control Design of Wide-Area Hypersonic Vehicle Based on Dynamic Inversion
The hypersonic vehicles (HV) represented by the combined powered aerospace vehicle have the characteristics of strong coupling, uncertain aerodynamic...
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A Finite-Time Partial Integrated Guidance and Control Approach for Formation of Autonomous Aerial and Ground Robots
Using the the philosophy of sliding mode control, a nonlinear partially integrated guidance and control (PIGC) method is proposed that guarantees...
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Fault-Tolerant Integrated Guidance and Control Design for Hypersonic Vehicle Based on ADRC
To ensure the stability and safety of hypersonic vehicle reentry flights, we have designed a fault-tolerant integrated guidance and control (FTIGC)...
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Online Sliding Mode-Based Integrated Guidance and Control System for a Quadcopter UAV in the Presence of Unknown Obstacles
This paper presents an integrated method of guidance and control for a quadcopter with nonlinear dynamics, which assumes to be under-actuated. The...
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Nonsingular Fixed-Time Integrated Guidance and Control
A backstep**-based nonsingular fixed-time integrated guidance and control strategy is proposed. To avoid the appearance of singular terms in the...
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A fuzzy adaptive controller design for integrated guidance and control of a nonlinear model helicopter
A fuzzy adaptive sliding mode controller is presented in this research and implemented on a nonlinear helicopter model. An integrated guidance and...
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Review on guidance and control of aerospace vehicles: recent progress and prospect
This paper expounds on the development status and relevant works of control and guidance methods of the aerospace vehicle in recent years. The...
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Time-Varying Sliding Mode-Based Integrated Guidance and Control Design
The problem of a missile attacking maneuvering targets has been considered in this paper.Meanwhile, a new integrated guidance and control (IGC)...
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6D trajectory, guidance and control development for air-breathing phase of reusable launch vehicle
This paper presents the development of 6D trajectory, integrated guidance and control algorithm for winged cone hypersonic air-breathing vehicle....
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Integrated Guidance and Control Design for Orbit Injection Phase of Launch Vehicle
This study develops a modified integrated guidance and control (IGC) design for the orbit injection phase of a launch vehicle. Firstly, a coupled...
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Review of Advanced Guidance and Control Methods
Over the past few decades, how to design a sophisticated guidance and control the (G &C) system for space and aerospace vehicles has been widely...
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Satellite Cluster Flight Using Guidance Trajectory and Model Predictive Control
This paper presents a model predictive control based framework that is used in conjunction with a polytope boundary constraint and the...
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Scalable guidance and control laws for model-scale analysis of autonomous ship landing systems
Due to the potential to expand flight envelopes and increase flight safety for sea-based rotorcraft, there has been a drive to produce reliable...
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Event-Based Guidance and Incremental Control with Application to Fixed-wing Unmanned Aerial Vehicle Perched Landing Maneuvers
Considering the nonlinearity and unknown dynamics of fixed-wing unmanned aerial vehicles in perched landing maneuvers, an event-based online guidance...
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Tracking Differentiation Guidance Law Based on Backstep** Control
This paper presents a tracking differentiation guidance law based on backstep** control method with the autopilot dynamics compensation. For...
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Analysis on the Key Technology of Guidance and Control of Missile and Gun Combined Air Defense Missile
Starting from the challenge of the guidance and control system posed by the battlefield environment and combat mission of the missile-gun integrated...
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Integrated attitude—orbit control of solar sail with single-axis gimbal mechanism
A new attitude control method for solar sails is proposed using a single-axis gimbal mechanism and three-axis reaction wheels. The gimbal angle is...
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Integrated Guidance and Control Design for Homing Missile with Terminal Angular Constraint
Aiming at homing missiles, an integrated guidance and control (IGC) design scheme is developed. Meanwhile, the situation of terminal angular...
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Integrated Optimal Guidance for Reentry and Landing of a Rocket Using Multi-Phase Pseudo-Spectral Convex Optimization
This paper proposes integrated optimal guidance for the reentry and landing of a rocket using the multi-phase pseudo-spectral convex optimization...
