Comprehensive Identi�cation from FrEquency Responses (CIFER®)

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 (ºÚ¹Ï³ÔÁÏÍøRF) 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:
- Identi�cation algorithms highly-exercised and tuned based on many
flight projects - Highly-flexible and interactive de�nition of identi�cation model structures
- Fully automated weighting function selection based on frequency-response accuracy
- Reliable parameter accuracy metrics
- Integrated procedure for identi�cation and model structure determination
- Time-domain veri�cation of models, including identi�cation of offsets
and biases
Application Modules within CIFER® Allow:
- Rapid identi�cation of transfer-function models
- Spectral signal analysis
- Handling-qualities and classical servoloop analysis
- Time- and frequency-domain comparisons of identi�cation versus simulation model prediction
Additional Information
SALES & OTHER INQUIRIES CONTACT
San José State University Research Foundation
flight-control-sta@sjsu.edu