APPLICATION OF ROBUST SYNTHESIS METHODOLOGY FOR SOUNDING ROCKET ATTITUDE STABILIZATION
Annotation
In this paper, the application of robust methodology for attitude stabilization of a sounding rocket is addressed. The unknown uncertainties are bounded and estimated. Stabilizing controller based on H-infinity optimisation and μ synthesis and analysis methods is designed while estimating the uncertainty model. The stability and performance levels of the control system are investigated at each estimate using computer simulation.
Keywords
Постоянный URL
Articles in current issue
- RADIO PERCEPTIBILITY OF ANTENNA WINDOWS OF HYPERSONIC AIRPLANE
- DATA CHARACTERISTICS OF THE MICROMECHANICAL GYROSCOPES BASED ON SILICON TECHNOLOGY MICROELECTROMECHANICAL SYSTEMS
- DIFFERENTIAL SENSITIVE ELEMENT ON SAW WITH SMALL CHANGE OF FREQUENCY AND PHASE CODING
- DISCRIMINATIVE METHOD OF IMPROVING THE MEASUREMENTS OF STAR COORDINATORS WITH CCD-MATRICES
- PRINCIPLES AND SYSTEMS OF HEAVY WIG-CRAFT FLIGHT CONTROL
- MATHEMATICAL MODELS OF A COMPLEX FLEXIBLE SPACE CONSTRUCTIONS AND SOFTWARE FOR DESIGN OF A CONTROL SYSTEMS
- CONTROL SYSTEMS OF SMALL-SIZED REMOTE-PILOTED AIRPLANES
- APPLICATION OF ROBUST SYNTHESIS METHODOLOGY FOR SOUNDING ROCKET ATTITUDE STABILIZATION
- SEMI-NATURAL MODELING OF PLANE SYSTEM ANTI-SLIDING AUTOMATICS
- METHOD OF THE ADAPTIVE OPTIMUM FILTRATION OF SIGNALS IN NAVIGATING COMPLEXES
- AUTONOMOUS RELATIVE NAVIGATION OF SPACECRAFTS WITH A SINGLE FREQUENCY GPS RECEIVER
- APPROACH TO STRUCTURE MODIFICATION SPECIFICATION OF ON-BOARD PROGRAM SUPPORT CODE