Wind tunnel test of an RPV with shape-change control effector and sensor arrays

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 3, Issue , 2004, Pages 1680-1690

  Raney, David L ^a,e   Cabell, Randolph H ^a,f   Barnwell, William G ^b   Lion, S Todd ^b   Sloan, Adam R ^c   Hautamaki, Bret A ^d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b North Carolina State University   (United States)

^c Department of Aeronautics and Astronautics Department of Mechanical Engineering and Industrial for Computational and Mathematical Engineering   (United States)

^d UNIVERSITY OF MICHIGAN   (United States)

^e Dynamics and Control Branch   (United States)

^f Structural Acoustics Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL EFFECTORS; MULTIFUNCTIONAL EFFECTOR AND SENSOR ARRAYS (MESA); REMOTELY PILOTED VEHICLES (RPV); SYNTHETIC JETS;

ARRAYS; BANDWIDTH; COMPUTER SIMULATION; FEEDBACK; FLIGHT DYNAMICS; REMOTE CONTROL; SENSORS; WIND TUNNELS;

JET AIRCRAFT;

EID: 19944401888     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Kroo, I.: "Aerodynamic Concepts for Future Aircraft," AIAA Paper 99-3 524, July 1999.
2. Park, M.A.; Green, L.L.; Montgomery, R.C.; Raney, D.L.: "Determination of Stability and Control Derivatives Using Computational Fluid Dynamics and Auto-made Differentiation", AIAA 99-3136, June 1999.
3. Padula, S.L.; Rogers, J.L.; Raney, D.L.: "Multidisciplinary Techniques and Novel Aircraft Control Systems", AIAA paper 2000-4848, April 2000.
4. Raney, D. L., Montgomery; R. C., Green, L.L.; Park, M. A.: "Flight Control using Distributed Shape-Change Effector Arrays," AIAA paper 2000-1560, April 2000.
5. Bieniawski, S.; Kroo, Ilan M.:"Flutter Suppression Using Micro-Trailing Edge Effectors", AIAA paper 2003-1941.
6. Lee, Hak-Tae; Kroo, Ilan M.; Bieniawski, S.: "Flutter Suppression for High Aspect Ratio Flexible Wings Using Microflaps", AIAA 2002-1717, 43rd AIAA Structures, Structural Dynamics and Materials Conf, April 2002.
7. Florance, J.P.; Burner, A.W.; G.A.; Hunter, C.A; Graves, S.S.;Martin, C.A.: "Contributions of the NASA Langley Research Center to the DARPA/AFRL/NASA/Northrop Grumman Smart Wing Program", No. 2003-1961, AIAA Dynamics Specialists Conf, April 2003, Norfolk, VA
8. Martin, C.A., et al.: "Design, Fabrication, and Testing of Scaled Wind Tunnel Model for Smart Wing Phase 2 Program", No. 4332-50, SPIE Symposium on Smart Structures and Materials, Newport Beach, CA, March 2001.
9. Wang, D. P.; Bartley-Cho, J.D.; Martin, C. A.; Hallam, B. J.: "Development of High-Rate, Large Deflection, Hingeless Trailing Edge Control Surface for the Smart Wing Wind Tunnel Model", Vol. 4332, pp.401-418, SPIE Symposium on Smart Structures and Materials, Newport Beach, CA, 5-8 March 2001.
10. Barnwell, William G.: "Distributed Actuation and Sensing on an Uninhabited Aerial Vehicle", Thesis for Master of Science in Aerospace Engineering at North Carolina State University, MAE Dept, August 2003.
11. Ashby, D. L., Dudley, M. R., Iguchi, S. K., Browne, L., Katz, J., "Potential Flow Theory and Operation Guide for the Panel Code PMARC," NASA TM-102851, Jan 1991.
12. Haykin, S.: Adaptive Filter Theory. Prentice Hall, 1991, Englewood Cliffs, NJ; ISBN 0-13-013236-5.
13. Rafaely, B.; Elliott, S. J.: "A Computationally Efficient Frequency-Domain LMS Algorithm with Constraints on the Adaptive Filter", IEEE Transactions on Signal Processing, Vol. 48, No. 6, June 2000, pp. 1649-1655.