Aircraft as adaptive nonlinear system which must be in the adaptational maximum zone for safety

Conference · Sat Dec 31 00:00:00 EST 1994

OSTI ID:482004

Ignative, M ^[1]; Simatos, N ^[2]; Sivasundaram, S ^[3]

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1. State Aerospace Instruments Academy, St. Petersburg (Russian Federation)
2. Apollo Aerospace International, Daytona Beach, FL (United States)
3. Embry-Riddle Aeronautical Univ., Daytona Beach, FL (United States)

Safety is a main problem in aircraft. We are considering this problem from the point of view related to existence of the adaptational maximum in complex developing systems. Safety space of aircraft parameters are determined. This space is transformed to different regimes of flight, when one engine malfunctions etc., are considered. Also it is shown that maximum safety is in adaptational maximum zone.

• OSTI ID: 482004
• Report Number(s): CONF-960503-; TRN: 97:002904-0036
• Resource Relation: Conference: 1. international conference on nonlinear problems in aviation and aerospace, Daytona Beach, FL (United States), 9-11 May 1996; Other Information: PBD: 1994; Related Information: Is Part Of First international conference on nonlinear problems in aviation & aerospace; Sivasundaram, S. [ed.]; PB: 729 p.
• Country of Publication: United States
• Language: English

Related Subjects

33 ADVANCED PROPULSION SYSTEMS
99 MATHEMATICS
COMPUTERS
INFORMATION SCIENCE
MANAGEMENT
LAW
MISCELLANEOUS
AIRCRAFT
ENGINEERED SAFETY SYSTEMS
COMPUTERIZED CONTROL SYSTEMS
NONLINEAR PROBLEMS
PARTIAL DIFFERENTIAL EQUATIONS
COMPUTER-AIDED INSTRUCTION