[go: up one dir, main page]

Pal et al., 2024 - Google Patents

Linear Parameter Varying Model-Based Predictive Trajectory Tracking Control of Quadrotor

Pal et al., 2024

Document ID
11964966977420324552
Author
Pal S
Deb A
Publication year
Publication venue
2024 11th International Conference on Signal Processing and Integrated Networks (SPIN)

External Links

Snippet

This paper incorporates a constrained Model Predictive Control (MPC) formulation for attitude control of an F450 Quadrotor that has potential of Linear Parameter Varying (LPV) modeling of the attitude subsystem to consider the change in system dynamics. The …
Continue reading at ieeexplore.ieee.org (other versions)

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
    • G05B13/042—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators in which a parameter or coefficient is automatically adjusted to optimise the performance
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B11/00—Automatic controllers
    • G05B11/01—Automatic controllers electric
    • G05B11/32—Automatic controllers electric with inputs from more than one sensing element; with outputs to more than one correcting element
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/0265—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric the criterion being a learning criterion
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00—Program-control systems
    • G05B2219/30—Nc systems
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
    • G05D1/0044—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement by providing the operator with a computer generated representation of the environment of the vehicle, e.g. virtual reality, maps
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/021—Control of position or course in two dimensions specially adapted to land vehicles
    • G05D1/0287—Control of position or course in two dimensions specially adapted to land vehicles involving a plurality of land vehicles, e.g. fleet or convoy travelling
    • G05D1/0291—Fleet control
    • G05D1/0295—Fleet control by at least one leading vehicle of the fleet

Similar Documents

Publication Publication Date Title
Noordin et al. Adaptive PID controller using sliding mode control approaches for quadrotor UAV attitude and position stabilization
Wang et al. Dynamics modelling and linear control of quadcopter
He et al. A simple attitude control of quadrotor helicopter based on Ziegler‐Nichols rules for tuning PD parameters
Lee et al. Control of complex maneuvers for a quadrotor UAV using geometric methods on SE (3)
Szafranski et al. Different approaches of PID control UAV type quadrotor
Herrera et al. Sliding mode control: An approach to control a quadrotor
Bou-Ammar et al. Controller design for quadrotor uavs using reinforcement learning
CN113759979B (en) Event-driven-based online track planning method for unmanned aerial vehicle hanging system
Rajappa et al. Adaptive super twisting controller for a quadrotor uav
Alsafadi et al. Synthesis of fuzzy controller based on simple PID controller
Razzaghian et al. Adaptive fuzzy sliding mode control for a model-scaled unmanned helicopter
Velagić et al. Design of LQR controller for 3D trajectory tracking of octocopter unmanned aerial vehicle
Duan et al. Attitude tracking control of small-scale unmanned helicopters using quaternion-based adaptive dynamic surface control
Shauqee et al. Quadrotor Controller Design Techniques and Applications Review.
Yamasaki et al. Integrated guidance and autopilot for a path-following UAV via high-order sliding modes
Weng et al. Fast quasi‐sliding mode control of unknown QUAVs: A data‐driven cascade control approach
Meradi et al. A predictive sliding mode control for quadrotor’s tracking trajectory subject to wind gusts and uncertainties
Dasgupta et al. A singularity-free hierarchical nonlinear quad-rotorcraft control using saturation and barrier lyapunov function
Pal et al. Linear Parameter Varying Model-Based Predictive Trajectory Tracking Control of Quadrotor
Miah et al. Generalized cascaded control technology for a twin-rotor MIMO system with state estimation
Xue et al. A Moving Target Tracking Control of Quadrotor UAV Based on Passive Control and Super‐Twisting Sliding Mode Control
Zeghlache et al. Adaptive type-2 fuzzy sliding mode control using supervisory type-2 fuzzy control for 6 DOF octorotor aircraft
Kumar et al. PFOID-SMC approach to mitigate the effect of disturbance and parametric uncertainty on the quadcopter
Ali et al. Control system analysis and design of quadcopter in the presence of unmodelled dynamics and disturbances
Reyad et al. An optimal PID controller for a qaudrotor system based on DE algorithm