[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Xu et al., 2018 - Google Patents

A suboptimal excitation torque for parameter estimation of a 5-DOF spacecraft simulator

Xu et al., 2018

Document ID
12638797342457969031
Author
Xu Z
Chen Y
Xu Z
Publication year
Publication venue
Advances in Space Research

External Links

Snippet

Five degrees of freedom spacecraft simulators are designed to verify spacecraft control strategies, rendezvous and docking techniques. The accurate knowledge of simulator inertia parameters which can be calculated by parameter estimation is of vital importance in these …
Continue reading at www.sciencedirect.com (other versions)

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
    • G01C21/10—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • 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
    • 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

Similar Documents

Publication Publication Date Title
Wu et al. Modeling and sliding mode-based attitude tracking control of a quadrotor UAV with time-varying mass
Philip et al. Relative position and attitude estimation and control schemes for the final phase of an autonomous docking mission of spacecraft
Hong Fuzzy logic based closed-loop strapdown attitude system for unmanned aerial vehicle (UAV)
Xu et al. Parameter estimation of a three-axis spacecraft simulator using recursive least-squares approach with tracking differentiator and Extended Kalman Filter
Salaris et al. Online optimal perception-aware trajectory generation
Avila et al. Experimental model identification of open-frame underwater vehicles
Wang et al. Tracking control for a velocity-sensorless VTOL aircraft with delayed outputs
Yoshida et al. Inertia parameter identification for a free-flying space robot
Takada et al. Control moment gyro singularity-avoidance steering control based on singular-surface cost function
Srivastava et al. Attitude determination and control system for a leo debris chaser small satellite
Zhang et al. Gyro-less angular velocity estimation and intermittent attitude control of spacecraft using coarse-sensors based on geometric analysis
Leeghim et al. Angular rate and alignment estimation for gyroless spacecraft by only star trackers
Warier et al. Line-of-sight based spacecraft attitude and position tracking control
Xu et al. A suboptimal excitation torque for parameter estimation of a 5-DOF spacecraft simulator
Espíndola et al. A four-DOF Lagrangian approach to attitude tracking
Toloei et al. Design of predictive control and evaluate the effects of flight dynamics on performance of one axis gimbal system, considering disturbance torques
CN108871312A (en) A kind of joint method for determining posture of gravity gradiometer and star sensor
Oh et al. Robust stabilization technique for the leader steering slung-load system/using sliding mode control
Brouk Propagation of uncertainty through coning, sculling, and scrolling corrections for inertial navigation
Xuan et al. From PID to L1 adaptive control for automatic balancing of a spacecraft three-axis simulator
Hajiyev et al. Integration of algebraic method and EKF for attitude determination of small information satellites
de Oliveira et al. Air bearing platforms for simulation of spacecraft attitude control systems
Tan et al. A new approach for small satellite gyroscope and star tracker fusion
Abeysekera et al. Modelling and implementation of PID control for balancing of an inverted pendulum
Habib Combined spacecraft orbit and attitude control through extended Kalman filtering of magnetometer, gyro, and GPS measurements