Decoupling trajectory tracking for gliding reentry vehicles

Zixuan Liang*, Zhang Ren, Xingyue Shao

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

21 Citations (Scopus)

Abstract

A decoupling trajectory tracking method for gliding reentry vehicles is presented to improve the reliability of the guidance system. Function relations between state variables and control variables are analyzed. To reduce the coupling between control channels, the multiple-input multiple-output (MIMO) tracking system is separated into a series of two single-input single-output (SISO) subsystems. Tracking laws for both velocity and altitude are designed based on the sliding mode control (SMC). The decoupling approach is verified by the Monte Carlo simulations, and compared with the linear quadratic regulator (LQR) approach in some specific conditions. Simulation results indicate that the decoupling approach owns a fast convergence speed and a strong anti-interference ability in the trajectory tracking.

Original languageEnglish
Article number7032913
Pages (from-to)115-120
Number of pages6
JournalIEEE/CAA Journal of Automatica Sinica
Volume2
Issue number1
DOIs
Publication statusPublished - 10 Jan 2015
Externally publishedYes

Keywords

  • Hypersonic
  • decoupling control
  • reentry vehicle
  • sliding mode control (SMC)
  • trajectory tracking

Fingerprint

Dive into the research topics of 'Decoupling trajectory tracking for gliding reentry vehicles'. Together they form a unique fingerprint.

Cite this