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NAME:
PII Scientific Package for Interactive Identification of Aircraft Aerodynamics Model
using unsteady flight and wind tunnel test data.
PRINCIPAL DEVELOPERS:
M. Goman, A. Khramtsovsky, S. Usoltsev, J. Vinogradov, S. Tyrtyshnikov.
SOFTWARE CAPABILITIES:
During motion of modern airplane at the high angles of attack stall and vortex flow are
developed. This makes identification of highly nonlinear aerodynamical characteristics
more complex because these characteristics exhibit essential dynamic properties. Since
the real aerodynamic model is unknown, the problem of identification is incorrect. It
makes necessary the inclusion of an expert into the process of identification. PII is
designed to automatize the process of identifications from one side and to allow for an
expert to participate in the identification process from the other side.
PII enables the following:
• account of a priori information, ability of data compatibility check;
• easy changing of the structure of aerodynamic model (from ordinary linear to
unsteady nonlinear) and investigation of its features, identifiability of parameters;
• using a number of methods for parameters estimation;
• verification of obtained aerodynamical model using a number of experimental data
sets.
INTERACTIVE CAPABILITIES:
Essential feature of this package is the possibility of interactive control of identification
process. This enables to avoid non-physical estimates of aerodynamic characteristics.
PROGRAMMING LANGUAGES USED:
Borland C++ ver. 3.0
COMPUTERS AND TERMINALS ON WHICH AVAILABLE:
IBM PC/AT compatible computers with EGA or VGA graphics cards.
DOCUMENTATION:
User Guide and Textbook in English.
SIZE OF THE PACKAGE:
≈ 60,000 lines of source code. IBM PC: 640kB of RAM, MS-DOS/PC-DOS ver. 3.30
or higher, package requires ≈ 1mB on hard disk drive.
STATE OF DEVELOPMENT:
Production code, installed and used in a number of institutions in Russia and abroad.
PERSON TO CONTACT FOR DETAILS:
Mikhail Goman
Central Aero-Hydrodynamics Institute (TsAGI)
140160, Zhukovsky–3, Moscow Region
Russia.
Fax (7-095) 271-00-19

2

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M.G.Goman et al (1994) - PII advertisement

  • 1. NAME: PII Scientific Package for Interactive Identification of Aircraft Aerodynamics Model using unsteady flight and wind tunnel test data. PRINCIPAL DEVELOPERS: M. Goman, A. Khramtsovsky, S. Usoltsev, J. Vinogradov, S. Tyrtyshnikov. SOFTWARE CAPABILITIES: During motion of modern airplane at the high angles of attack stall and vortex flow are developed. This makes identification of highly nonlinear aerodynamical characteristics more complex because these characteristics exhibit essential dynamic properties. Since the real aerodynamic model is unknown, the problem of identification is incorrect. It makes necessary the inclusion of an expert into the process of identification. PII is designed to automatize the process of identifications from one side and to allow for an expert to participate in the identification process from the other side. PII enables the following: • account of a priori information, ability of data compatibility check; • easy changing of the structure of aerodynamic model (from ordinary linear to unsteady nonlinear) and investigation of its features, identifiability of parameters; • using a number of methods for parameters estimation; • verification of obtained aerodynamical model using a number of experimental data sets. INTERACTIVE CAPABILITIES: Essential feature of this package is the possibility of interactive control of identification process. This enables to avoid non-physical estimates of aerodynamic characteristics. PROGRAMMING LANGUAGES USED: Borland C++ ver. 3.0 COMPUTERS AND TERMINALS ON WHICH AVAILABLE: IBM PC/AT compatible computers with EGA or VGA graphics cards. DOCUMENTATION: User Guide and Textbook in English. SIZE OF THE PACKAGE: ≈ 60,000 lines of source code. IBM PC: 640kB of RAM, MS-DOS/PC-DOS ver. 3.30 or higher, package requires ≈ 1mB on hard disk drive.
  • 2. STATE OF DEVELOPMENT: Production code, installed and used in a number of institutions in Russia and abroad. PERSON TO CONTACT FOR DETAILS: Mikhail Goman Central Aero-Hydrodynamics Institute (TsAGI) 140160, Zhukovsky–3, Moscow Region Russia. Fax (7-095) 271-00-19 2