A flight control design of a re-entry vehicle using a double-loop control system with fuzzy gain-scheduling

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 215, Issue 1, 2001, Pages 1-12

  Fujimori, A ^a   Nikiforuk, P N ^b   Gupta, M M ^b  

^a SHIZUOKA UNIVERSITY   (Japan)

^b UNIVERSITY OF SASKATCHEWAN   (Canada)

Author keywords

Double loop; Flight control; Gain scheduling; Re entry vehicle

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; EIGENVALUES AND EIGENFUNCTIONS; EQUATIONS OF MOTION; FUZZY SETS; LINEAR EQUATIONS; NAVIGATION; REENTRY; STABILITY; STATE FEEDBACK; TRAJECTORIES;

AUTOMATIC LANDING FLIGHT EXPERIMENT VEHICLE; DOUBLE LOOP CONTROL SYSTEM; FLIGHT CONTROL; FUZZY GAIN SCHEDULING; INNER LOOP CONTROL LAW; OUTER LOOP CONTROL LAW; REENTRY VEHICLE;

SPACECRAFT;

EID: 0035043141     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/0954410011531709     Document Type: Conference Paper

References (10)

1. NASDA pins its hopes on HOPE
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