Aircraft reconfiguration using neural generalized predictive control

Proceedings of the American Control Conference

Volumn 4, Issue , 2001, Pages 2924-2929

  Soloway, Don ^a   Haley, Pam ^b  

^a NASA AMES RESEARCH CENTER   (United States)

^b NASA Lungley Research Center   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DEGREES OF FREEDOM (MECHANICS); FAILURE ANALYSIS; FLIGHT DYNAMICS; NEURAL NETWORKS; REAL TIME SYSTEMS; SPACE RESEARCH; SYSTEM STABILITY; TRANSPORT AIRCRAFT;

AIRCRAFT RECONFIGURATION; COMMERCIAL AIRCRAFT; CONTROL PITCH RATE; NEURAL GENERALIZED PREDICTIVE CONTROL; SYMMETRIC AILERON DEFLECTIONS;

PREDICTIVE CONTROL SYSTEMS;

EID: 0034842131     PISSN: 07431619     EISSN: None     Source Type: Journal    
DOI: 10.1109/ACC.2001.946348     Document Type: Article

References (6)

1. Implementation and flight test assessment of an adaptive reconfigurable flight control system
2. Direct adaptive reconfigurable control of a tailless fighter aircraft
3. Reconfigurable flight control using nonlinear dynamic inversion with a special accelerometer implementation
4. Neural generalized predictive control: A newton-raphson implementation
5. Realtime adaptive control using neural generalized predictive control
6. The NASA advanced concepts flight simulator: A unique transport aircraft research environment