OPTIMIZATION OF FLYING VEHICLE DYNAMICS WITH DIFFERENT CRITERI
Annotation
The problem of optimal control over a flying vehicle regarded as a hard body is considered. Flying object dynamics is described by Euler and Poisson equations. The optimal solution to the problem is obtained on the base of Pontriagin principle with Lagrange criterion as a goal functional.
Keywords
Постоянный URL
Articles in current issue
- CLUSTER NUMBER ESTIMATION PROBLEM IN PARTITION METHO
- CREATION OF A COMMON INFORMATIONAL RESOURCE OF CORPORATE NETWORK IN SOCIAL ORGANIZATIONAL-TECHNICAL SYSTEM
- MEDICAL DATA-MEASURING SYSTEM FOR FUNCTIONAL DIAGNOSTICS
- ESTIMATION OF TOLERANCES ON COMPONENTS IN TECHNICAL REALIZATION OF CONTROL LAWS
- OPTIMIZATION OF FLYING VEHICLE DYNAMICS WITH DIFFERENT CRITERI
- AN INTELLECTUAL AGENT FOR SEMANTIC WEB
- A METHOD TO REVEAL UNDECLARED PERFORMANCE CAPABILITIES AND VALUES “DON’T CARE” OF A CALCULATION PROCEDURE
- ALGORITHMS OF PARAMETRICAL IDENTIFICATION OF ELECTROMECHANICAL SYSTEMS PROTECTED AGAINST HINDRANC
- TECHNIQUE FOR MEASURING THE TIME CONSTANT OF ELECTRIC DRIVE
- CIRCULAR GENERATOR ON PROGRAMMABLE LOGICAL INTEGRATED CHIP
- PARAMETERS OF SPHERICALLY SYMMETRIC DISTRIBUTION OF REFRACTIVE INDEX IN SPHERICAL AND CARTESIAN COORDINATE SYSTEMS
- APPLICATION OF INTEGRATED CRITERIA OF EFFICIENCY IN LASERS DEVELOPMENT AND EXPLOITATION
- ELECTRO-OPTICAL MODULATOR FOR FIBER OPTIC COMMUNICATION LINE