Verifying pilot gain in PIO flight test (2007)
- Authors:
- USP affiliated authors: VAROTO, PAULO SERGIO - EESC ; MACIEL, CARLOS DIAS - EESC
- Unidade: EESC
- Subjects: CONTROLE DE AERONAVES; PILOTAGEM DE AERONAVES; PROCESSOS COGNITIVOS
- Language: Inglês
- Abstract: A validation method for synthetic tracking task PIO flight test is introduced. The theory is based on the entropy concept from information theory and on the structural pilot model of the human pilot. The method is presented for single axis pilot tracking maneuvers and offers a measure of the human pilot gain employed during its execution. Linear aircraft dynamics is used to model the plant. Flight test data from a FAR-25 transport aricraft is used to verify the theory of how to determine a measure of the ratio bethween time spent by the human pilot in the error loop versus in the error rate loop to control the aircraft. This measure is proposed as a test point validation method for PIO flight testing
- Imprenta:
- Conference titles: AIAA Atmospheric Flight Mechanics Conference and Exhibit
-
ABNT
CELERE, André Luís e VAROTO, Paulo Sérgio e MACIEL, Carlos Dias. Verifying pilot gain in PIO flight test. 2007, Anais.. Reston: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2007. . Acesso em: 06 fev. 2026. -
APA
Celere, A. L., Varoto, P. S., & Maciel, C. D. (2007). Verifying pilot gain in PIO flight test. In . Reston: Escola de Engenharia de São Carlos, Universidade de São Paulo. -
NLM
Celere AL, Varoto PS, Maciel CD. Verifying pilot gain in PIO flight test. 2007 ;[citado 2026 fev. 06 ] -
Vancouver
Celere AL, Varoto PS, Maciel CD. Verifying pilot gain in PIO flight test. 2007 ;[citado 2026 fev. 06 ] - Análise modal no domínio da frequência: um método de identificação multi-modos
- Estudo da vibração de um dispositivo piezelétrico não linear para geração de energia
- Estudo de geradores piezoelétricos não-lineares
- On the force drop off phenomenon in shaker testing in experimental modal analysis
- Rules for the exchange and analysis of dynamic information: part II : numerically simulated results for a deterministic excitation with no external loads
- Rules for the exchange and analysis of dynamic information: part V : Q-transmissibility matrix vs. single point transmissibility in test environments
- Rules for the exchange and analysis of dynamic information: part IV : numerically simulated and experimental results for a Random excitation
- Model for force transducer bending moment sensitivity and response during calibration
- 'FE' study of the exciter - structures interaction in vibration testing
- Environmental testing, implementation
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
