Journal
Scientific and technical journal «Priborostroenie»
UDK519.7
Issue:1 (58)
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ADAPTIVE CONTROL OVER LATERAL MOVEMENT OF AIRCRAFT IN THE LANDING MODE
Annotation
A solution to the problem of adaptive control over lateral movement of aircraft in the landing mode is proposed. The control system with a reference model based on modified algorithm of high order adaptation is developed. Simulation results are presented to illustrate the efficiency of the synthesized algorithm.
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Articles in current issue
- ANALYSIS OF CURRENT STATE AND PROSPECT FOR THE DEVELOPMENT OF BOKZ STAR TRACKERS FAMILY
- AUTONOMOUS NAVIGATION SYSTEM OF SMALL SPACECRAFT
- ALGORITHM OF DYNAMICAL ESTIMATION OF OBJECT ORIENTATION PARAMETERS FROM SATELLITE MEASUREMENTS
- AMBIGUITY RESOLUTION OF PHASE MEASUREMENTS AND SELECTION OF CARRIER FREQUENCIES IN SATELLITE NAVIGATING SYSTEM
- ESTIMATION OF ACCURACY CHARACTERISTICS OF CARRIER ROCKET CONTROL SYSTEM BY RESULTS OF LAUNCHES UNDER VARIOUS CONDITIONS
- DISPLACEMENT CONTROL IN OPTICAL-ELECTRONIC SYSTEMS WITH OPTICAL EQUISIGNAL ZONE
- DETERMINATION OF OPTICAL COMPONENTS BASIC PARAMETERS OF OPTICAL SYSTEM WITH VARIABLE MAGNIFICATION
- PROBABILISTIC ANALYSIS OF DATA GATHERING AND PROCESSING CENTER OPERATION
- CREATION OF ANALYTIC SIGNAL WITH A KNOWN ELEMENTARY PHASE
- EFFECTIVE METHOD OF ACCELERATED LIFE TEST OF FRICTION ASSEMBLY
- PERMANENT MAGNET SYNCHRONOUS MOTOR TORQUE
- MODEL OF VISUAL MEASUREMENTS
- FIVE-LAYER QUARTER-WAVE ANTIREFLECTION COATING ON THE BASE OF THREE FILM-FORMING MATERIALS
- APPLICATION OF MATLAB SOFTWARE IN EDUCATIONAL PROCESS FOR MODELING OF MECHATRONIC SYSTEMS