Improved coupled force and moment parameter estimation for aircraft

24th Atmospheric Flight Mechanics Conference

Volumn , Issue , 1999, Pages 484-492

  Lee, Dong Chan ^a   Nagatif, M G ^a  

^a Wichita State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; FLIGHT DYNAMICS; FLIGHT SIMULATORS; TESTING; WIND TUNNELS;

AERODYNAMIC FORCES; AIRCRAFT MOTION; CONTROL DERIVATIVES; EQUATION ERROR METHOD; HIGH ANGLE OF ATTACK; MODELING FEATURES; STATE-DEPENDENT; STATIC WIND TUNNELS;

AERODYNAMICS;

EID: 84960501633     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Jaramillo, P. T. and Nagati, M. G., “A Multi­Point Approach for Aerodynamic Modeling in Complex Flow-Fields”, Journal of Aircraft,” Vol. 32, No. 6, Nov.-Dec. 1995, pp. 1335-1341
2. Jaramillo, P. T., Cho, Yongseung and Nagati, M. G., “Validation of a Multi-Point Approach for Modeling Spin Aerodynamics,” Journal of Aircraft, Vol. 32, No. 6, Nov.-Dec. 1995, pp. 1409-1412.
3. Jaramillo, P. T., Cho, Yongseung, and Nagati, M.G., “Application of a Multi-Point Model for Parameter Estimation, in Spins” Presented at the 1995 AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV., Jan. 1995, AIAA Paper 95­0341.
4. Cho, Yongseung, Nagati, M. G. and Jaramillo, P. T., “Parameter Estimation with a Multi-Point Model,” Presented at the 1995 AIAA Atmospheric Flight Mechanics Conference, Baltimore, MD, Aug. 1995, AIAA Paper 95-3498.
5. Cho, Y., and Nagati, M. G., “Coupled Force and Moment Parameter Estimation for Aircraft’, Journal of Aircraft, Vol. 35, No. 2, 1998, pp. 247-­253.
6. Stough, H. Paul El, et al., “Flight Investigation of the Effect of Tail Configuration on Stall, Spin and Recovery Characteristics of a Low-Wing General Aviation Research Airplane,” NASA TP-2644, 1987.
7. Bihrle, W. Jr., Barnhart, B., and Pantason, P., “Static Aerodynamic Characteristics of a Typical Single-Engine Low Wing General Aviation Design for an Angle of Attack Range of -8° to 90°" NASA CR-2971, July 1978.
8. Courtland D. Perkins and Robert E. Hage, “Airplane Performance Stability and Control,” John Wiley & Sons, Inc., 1957