Finite-Time Spacecraft’s Soft Landing on Asteroids Using PD and Nonsingular Terminal Sliding Mode Control
This paper presents a continuous control law of probe, which consists of PD (proportional-derivative) controller and nonsingular terminal sliding mode controller for probe descending and landing phases, respectively, in the case of the asteroid irregular shape and low gravity. The probe dynamic mode...
Main Authors: | Keping Liu, Fengxia Liu, Shenquan Wang, Yuanchun Li |
---|---|
Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2015-01-01
|
Series: | Mathematical Problems in Engineering |
Online Access: | http://dx.doi.org/10.1155/2015/510618 |
Similar Items
-
Adaptive Fuzzy Sliding Mode Control for the Probe Soft Landing on the Asteroids with Weak Gravitational Field
by: Yuanchun Li, et al.
Published: (2015-01-01) -
Disturbance Observer-Based Nonsingular Terminal Sliding Mode Control for Spacecraft Electromagnetic Docking
by: Jinghui Zhang, et al.
Published: (2020-01-01) -
Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults
by: Chenghu Jing, et al.
Published: (2019-01-01) -
Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems
by: Xiaohan Lin, et al.
Published: (2020-01-01) -
Attitude Analysis and Robust Adaptive Backstepping Sliding Mode Control of Spacecrafts Orbiting Irregular Asteroids
by: Chunhui Liang, et al.
Published: (2014-01-01)