1 |
Hummel, D., 'The Use of Aircraft Wakes to Achieve Power Reductions in Formation Flight', The Characterisation & Modification of Wakes from Lifting Vehicles in Fluids, AGARD Conference Proceedings 584, The Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine, France, 1996, pp. 36.1-36.13
|
2 |
Wagner, G., Jacqeus, D., Blake, W., and Pachter, M., ' Flight Test Results of Close Formation Flight For Fuel Savings', AIAA Atmospheric Flight Mechanics Conference and Exhibit, Monterey, CA, USA, August 2002
|
3 |
Wagner, G., Jacqeus, D., Blake, W., and Pachter, M., ' An Analytical Study of Drag Reduction in Tight Formation Flight', AIAA Atmospheric Flight Mechanics Conference and Exhibit, Montreal, Qebec, Canada, August 2001
|
4 |
Pachter, M., D'Azzo, J. J., and Proud, A. W., 'Tight Formation Flight Control', Journal of Guidance, Control, and Dynamics,Vol. 24, No. 2, 2001, pp. 246-254
DOI
ScienceOn
|
5 |
Chichka, D. F., Speyer, J. L., Fanti, D., and Park, C. G., 'Peak-Seeking Control for Drag Reduction in Formation Flight', Journal of Guidance, Control, and Dynamics, Vol. 29, No. 5, 2006, pp. 1221-1230
DOI
ScienceOn
|
6 |
Raymer, D. P., Aircraft Design : A Conceptual Approach, AIAA, Washington, DC, 1989, chaps.3,17,appendix A.4-2
|
7 |
Segal, S., Ben-Asher, J. Z., and Weiss, H., 'Derivation of Formation - Flight Guidance Laws for Unmanned Air Vehicles', Journal of Guidance, Control, and Dynamics, Vol. 28, No. 4, 2005, pp. 733-742
DOI
ScienceOn
|
8 |
Boskovic, J. D., Li, S. M., and Mehra, R. K., 'Semi-Globally Stable Formation Flight Control Design in Three Dimensions', Proceedings of the 40th IEEE Conference on Decision and Control, Orlando, FL, USA, December 2001
|