Integrated flight and propulsion control system design for a business jet

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2000, Pages

  Griswold, John ^a  

^a Raytheon Aircraft Company   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); JET AIRCRAFT; LONGITUDINAL CONTROL; PROPULSION; SYSTEMS ANALYSIS;

AUTOMATIC FLIGHT; COMBINED SYSTEM; DIRECTIONAL CONTROL; ENERGY PRINCIPLES; GAIN TUNING; PILOT WORKLOAD; PROPULSION CONTROL SYSTEMS; SIX DEGREE-OF-FREEDOM;

FLIGHT CONTROL SYSTEMS;

EID: 85088346113     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4542     Document Type: Conference Paper

References (6)

1. Bruce, K. R., "NASA B737 Flight Test Results of the Total Energy Control System", NASA CR- 178285, January, 1987.
2. Code of Federal Regulations, Advisory Circular AC 120-41: Criteria for Operational Approval of Airborne Windshear Alerting and Flight Guidance Systems, United States Government Printing Office, 1998.
3. st Annual NASA Aircraft Controls Workshop, October, 1983.
4. Lambregts, A. A., "Integrated System Design for Flight and Propulsion Control Using Total Energy Principles", American Institute of Aeronautics and Astronautics paper 83-2561, October, 1983.
5. Lambregts, A. A., "Operational Aspects of the Integrated Vertical Flight Path and Speed Control System", Society of Automotive Engineers paper 831420, October 1983.
6. Neal Barr, Dagfinn Gangsass, and Dwight R. Schaeffer, "Wind Models for Flight Simulator Certification of Landing and Approach Guidance and Control Systems", Unites States Department of Transportation, Federal Aviation Administration report FAA-RD-74-206, 1974.