A roll autopilot for autonomous air refueling

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Johnson, Kenneth L ^a   Awni, Kahtan A ^a  

^a UNIVERSITY OF KANSAS   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR MOBILITY; AIR NAVIGATION; AIRCRAFT; ERROR COMPENSATION; FLIGHT DYNAMICS; PLANFORMS; ROOT LOCI; VIBRATION CONTROL; WAKES;

DESIGN PROCEDURE; DISCRETE FREQUENCIES; LATERAL ACCELERATION CONTROL; LATERAL POSITIONS; LIFT COEFFICIENT; PROPORTIONAL PLUS DERIVATIVES; PROPORTIONAL PLUS INTEGRALS; ROOT LOCUS METHOD;

AIR REFUELING;

EID: 85088343383     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4752     Document Type: Conference Paper

References (3)

1. Trosen, D W et al,: "Development of an air-to-air refueling automatic flight control system using Quantitative Feedback Theory", AIAA Guidance, Navigation and Control Conference, Scottsdale, AZ, Aug. 1-3, 1994, Technical Papers. Pt. 1 (A94029961 e cockpit1 w0o-6u3ld), b Washington, DC, American Institute of Aeronautics and Astronautics, Report Number AIAA Paper 94-3545, 1994, p. 28-38.
2. Trochalidis, Vassilios,: "Aircraft aerodynamics and stability and control during air-to-air refueling (Ph.D. Thesis)", AIAA Technical Library, Report number AERO-REPT-9017; ETN-92-90940, Publication Date 19900500.
3. Bloy, A W et al,: "The lateral dynamic stability and control of a large receiver aircraft during air-to-air refueling", Aeronautical Journal, vol. 90, Jun-Jul 1986, p. 237-243.