Comprehensive Identi�cation from FrEquency Responses (CIFER®)

An ariel photo of a Comprehensive Identi�cation from FrEquency Responses

Figure: Comprehensive Identi�cation from FrEquency Responses

System identi�cation is a procedure by which a mathematical description of vehicle or component dynamic behavior is extracted from test data. System identi�cation can be thought of as an inverse of simulation. Simulation requires the adoption of (a-priori) engineering assumptions to allow the formulation of model equations. These simulation models are then used to predict aircraft or subsystem motion. In contrast, system identi�cation begins with measured aircraft motion and "inverts" the responses to rapidly extract a model which accurately reflects the measured aircraft motion, without making a-priori assumptions or requiring a time-consuming modeling effort. Applications of system identi�cation results include:
(1) comparison of wind tunnel and flight characteristics; (2) validation and update of simulation models; (3) handling-qualities analyses and speci�cation compliance; (4) optimization of automatic flight control systems; and (5) vibration and aeroelastic analyses.

The U.S. Army Combat Capabilities Development Command (DEVCOM) Aviation & Missile Center (AvMC) and San José State University Research Foundation (91°µÍøRF) jointly distribute an integrated facility for system identiï¬�cation based on a comprehensive frequency-response approach that is uniquely suited to the difï¬�cult problems associated with flight-test data analysis. The foundation of the CIFER® approach is the high-quality extraction of a complete multi-input/multi-output (MIMO) set of non-parametric input-to-output frequency responses. These responses fully characterize the coupled characteristics of the system without a-priori assumptions. Advanced Chirp-Z transform and composite optimal window techniques developed and exercised with over 10 years of flight project applications provide signiï¬�cant improvement in frequency-response quality relative to standard Fast Fourier Transforms (FFTs). Sophisticated nonlinear search algorithms are used to extract a state-space model which matches the complete input/output frequency-response data set.

Key Features of the CIFER® Approach Are:

  • Identiï¬�cation algorithms highly-exercised and tuned based on many
    flight projects
  • Highly-flexible and interactive deï¬�nition of identiï¬�cation model structures
  • Fully automated weighting function selection based on frequency-response accuracy
  • Reliable parameter accuracy metrics
  • Integrated procedure for identiï¬�cation and model structure determination
  • Time-domain veriï¬�cation of models, including identiï¬�cation of offsets
    and biases

Application Modules within CIFER® Allow:

  1. Rapid identi�cation of transfer-function models
  2. Spectral signal analysis
  3. Handling-qualities and classical servoloop analysis
  4. Time- and frequency-domain comparisons of identi�cation versus simulation model prediction

Additional Information

CIFER® Technical Papers


SALES & OTHER INQUIRIES CONTACT
San José State University Research Foundation 
flight-control-sta@sjsu.edu