Nonlinear Aerodynamic Model Development and Extraction from Flight Test Data for the S-3B Viking

Abstract

This paper addresses applied procedures for nonlinear aerodynamic model development and extraction from flight data for the S-3B Viking aircraft. The entire analysis procedures, from dynamic flight test data management to final blending and validation of the upgraded aerodynamic model, was performed within the Integrated Data Evaluation and Analysis Systems (IDEAS) developed by SAIC. IDEAS is a powerful database management system and analysis software containing a full complement of flight data preprocessing, calibration, simulation, model estimation, model verification, and validation tools.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2000
Accession Number
ADA384281

Entities

People

  • Alfonso Paris
  • Omeed Alaverdi

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aeronautics
  • Aircrafts
  • Algorithms
  • Calibration
  • Control Surfaces
  • Database Management Systems
  • Databases
  • Dynamic Pressure
  • Extraction
  • Flight
  • Landing Gear
  • Measurement
  • Preprocessing
  • Simulations
  • Trim Tabs
  • Validation

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aerospace Test and Evaluation
  • Computational Fluid Dynamics (CFD)