Multicriteria Parametrical Identification of the Parafoil-Load Delivery System
MetadataShow full item record
This paper addresses the problem of multicriteria (versus single-criterion) parametrical identification of the autonomously controlled cargo parafoil. Based on the structural identification as an initial step toward creation of an adequate model of the parafoil, a high-fidelity model including several dozens of optimization parameters has been developed. The present paper proposes the correct statement of the multicriteria parametrical identification problem including the necessity to investigate the feasible set of variable parameters. The paper advocates the use of the Parameter Space Investigation method and Multicriteria Optimization / Vector Identification software package to solve the problem.
18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, Munich, Germany, May 23-26, 2005.
RightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
Showing items related by title, author, creator and subject.
Statnikov, R.B.; Bordetsky, A.; Statnikov, A. (2005);The majority of engineering problems are essentially multicriteria. These criteria are usually contradictory. That is why specialists experience significant difficulties in correctly stating engineering optimization ...
Statnikov, R; Bordetsky, A.; Statnikov, A.; Yanushkevich, I. (Elsevier, 2006);Applied optimization problems such as design, identification, design of controlled systems, operational development of prototypes, analysis of large-scale systems, and forecasting from observational data are multicriteria ...
L1 Adaptive Flight Control System: Systematic Design and Verification and Validation of Control Metrics Xargay, Enric; Hovakimyan, Naira; Dobrokhodov, Vladimir; Statnikov, Roman B.; Kaminer, Isaac; Cao, Chengyu; Gregory, Irene M. (2010-08);This paper presents preliminary results of the application of the Parameter Space Investigation method for the design of the L1 flight control system implemented on the two turbine-powered dynamically-scaled GTM AirSTAR ...