H. Vo and S. Seshagiri, Robust control of f-16 lateral dynamics. Industrial Electronics, 34th Annual Conference of IEEE, pp.343-348, 2008.

N. Bandu, T. A. Pamadi, N. J. Neirynck, P. V. Hotchko, W. I. Tartabini et al., Simulation and analyses of stage separation of two-stage reusable launch vehicles, Journal of Spacecraft and Rockets, vol.44, pp.66-80, 2007.

N. Bandu, T. A. Pamadi, P. F. Neirynck, N. Covell, D. Hotchko et al., Simulation and analyses of staging maneuvers of next generation reusable launch vehicles. AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2004.

N. Bandu, P. V. Pamadi, M. D. Tartabini, C. M. Toniolo, C. Roithmay et al., Application of cfe/post2 for simulation of launch vehicle stage separation, AIAA Atmospheric Flight Mechanics Conference, 2009.

J. Gary, J. C. Balas, K. Doyle, A. Glover, R. Packard et al., µ -analysis and synthesis toolbox: Users guide version 3, 1993.

J. Reiner, G. J. Balas, and W. L. Garrard, Flight control design using robust dynamic inversion and time-scale separation, Automatica, vol.32, issue.11, pp.1493-1504, 1996.
DOI : 10.1016/S0005-1098(96)00101-X

H. Stephen, R. F. Lane, and . Stengel, Flight control design using non-linear inverse dynamics, American Control Conference, pp.587-596, 1986.

O. Harkegard, Flight Control Design Using Backstepping, 2001.

T. I. Fossen, Guidance and Control of Ocean Vehicles, 1994.

L. Sonneveldt, Nonlinear F-16 Model Description, 2006.

H. Peter and . Zipfel, Modeling and Simulation of Aerospace Vehicle Dynamics, 2001.

L. T. Nguyen, M. E. Ogburn, and P. Deal, Simulator study of fighter airplane with relaxed longitudinal static stability, 1979.

A. Nazmi, H. K. Mahmoud, and . Khalil, Robust control for a nonlinear servomechanism problem, International Journal of Control, vol.66, pp.779-802, 1997.

K. Hassan and . Khalil, On the design of robust servomechanisms for minimum phase nonlinear systems, Robust Nonlinear Control, vol.10, pp.339-361, 2000.

G. Damm, . Van-cuong, and . Nguyen, Mimo conditional integrator control for a class of nonlinear systems, proceedings of System Theory, Control, and Computing (ICSTCC) 15th International Conference, 2011.
URL : https://hal.archives-ouvertes.fr/hal-00744995

S. Seshagiri and H. K. Khalil, Robust output feedback regulation of minimum-phase nonlinear systems using conditional integrators, Automatica, vol.41, pp.43-54, 2005.

B. Charlet, J. Levine, and R. Marino, On dynamic feedback linearization, Systems & Control Letters, vol.13, issue.2, pp.143-151, 1989.
DOI : 10.1016/0167-6911(89)90031-5

B. Charlet, J. Levine, and R. Marino, Dynamic feedback linearization with application to aircraft control, Proceedings of the 27th IEEE Conference on Decision and Control, pp.701-705, 1988.
DOI : 10.1109/CDC.1988.194400

B. Charlet, J. Levine, and R. Marino, NEW SUFFICIENT CONDITIONS FOR DYNAMIC FEEDBACK LINEARIZATION, IFAC Symposium Capri, 1989.
DOI : 10.1016/B978-0-08-037022-4.50013-2

H. Nijmeijer, A. J. Van, and . Schaft, Nonlinear dynamical control systems, 1990.
DOI : 10.1007/978-1-4757-2101-0

B. Charlet, J. Levine, and R. Marino, Sufficient conditions for dynamic feedback linearization, SIAM Journal of Control and Optimization, 1991.

A. Tornambé, High-gain observers for non-linear systems, International Journal of Systems Science, vol.5, issue.9, pp.1475-1489, 1992.
DOI : 10.1016/0167-6911(87)90021-1

E. Bullinger and F. Allgower, An adaptive high-gain observer for nonlinear systems, Proceedings of the 36th IEEE Conference on Decision and Control, pp.4348-4353, 1997.
DOI : 10.1109/CDC.1997.649541

M. Sarigul-klijn and N. Sarigul-klijn, A study of air launch methods for RLVs, AIAA Space 2001 Conference and Exposition, 2001.
DOI : 10.2514/6.2001-4619

M. Burlacu and J. Kohlenberg, An analysis of the nanosatellites launches between, 3rd International Conference on Systems and Networks Communications, pp.292-297, 2004.
URL : https://hal.archives-ouvertes.fr/hal-01394109

M. Sarigul-klijn and N. Sarigul-klijn, Selection of a Carrier Aircraft and a Launch Method for Air Launching Space Vehicles, AIAA SPACE 2008 Conference & Exposition, 2008.
DOI : 10.2514/6.2008-7835

C. Gary and . Hudson, Quickreach responsive launch system, 4th Responsive Space Conference, 2006.

C. Dan, F. , and C. Webber, Falcon quickreach -airdrop envelope expansion to enable low cost space acces. Air Force Flight Test Center, 2005.

D. Facktor-lepore and D. Ewig, Results of quickreach small launch vehicle propulsion testing and next steps to demonstration flights, Utah State Small Satellite Conference, 2008.

D. Facktor-lepore and J. Padavano, Progress toward first flight of the quickreach small launch vehicle, Utah State Small Satellite Conference, 2007.

D. Facktor-lepore and J. Padavano, Airlaunch's quickreach small launch vehicle: Operationally responsive access to space, 15th Annual AIAA/USU Conference on Small Satellites, 2006.

J. Lopata and B. Rutan, Rascal -a demonstration of operationally responsive space launch. 2nd Responsive Space Conference, 2004.

J. Magni, S. Bennani, and J. Terlouw, Robust Flight Control : A Design Challenge, 1997.
DOI : 10.1007/BFb0113842

E. Trélat, Commande optimale. Notes du cours A08, 2008.

S. Seshagiri and H. K. Khalil, Output feedback regulation of minumumphase nonlinear systems using conditional integrators, Automatica, vol.41, pp.43-54, 2005.

S. Seshagiri and H. K. Khalil, Robust output regulation of minimum phase nonlinear systems using conditional servocompensators, International Journal of Robust and Nonlinear Control, vol.44, issue.2, pp.83-102, 2005.
DOI : 10.1002/rnc.977

Y. Attaullah, H. K. Memona, and . Khalil, Output regulation of nonlinear systems using conditional servocompensators, Automatica, vol.46, pp.1119-1128, 2010.

G. Damm, . Van-cuong, and . Nguyen, Mimo conditional servo-compensator control for a class of nonlinear systems (accepted), Proceedings of the 51th Conference on Decision and Control, 2012.

K. Hassan and . Khalil, Nonlinear Systems, 2001.
URL : https://hal.archives-ouvertes.fr/hal-00811192

R. Marino and P. Tomei, Nonlinear Control Design: Geometric, Adaptive and Robust, 1995.

A. Isidori, Nonlinear Control Systems, 1995.

S. Seshagiri and E. Promtun, Sliding mode control of F-16 longitudinal dynamics, 2008 American Control Conference, pp.1770-1775, 2008.
DOI : 10.1109/ACC.2008.4586748

E. Morelli, Global nonlinear parametric modeling with application to f-16 aerodynamics, Proceedings of the 1998 American Control Conference, pp.997-1001, 1998.

A. Young, C. Cao, and N. Hovakimyan, An Adaptive Approach to Nonaffine Control Design for Aircraft Applications, AIAA Guidance, Navigation, and Control Conference and Exhibit, pp.21-24, 2006.
DOI : 10.2514/6.2006-6343

S. Seshagiri and H. Khalil, On introducing integral action in sliding mode control, Proceedings of the 41st IEEE Conference on Decision and Control, 2002., pp.1473-1478, 2002.
DOI : 10.1109/CDC.2002.1184727

G. Meyer, R. Su, and L. R. Hunt, Application of nonlinear transformations to automatic flight control, Automatica, vol.20, issue.1, pp.103-107, 1984.
DOI : 10.1016/0005-1098(84)90069-4

S. Brian, L. , L. Frank, and L. , Aircraft Control and Simulation, 1992.

J. Roskam, Airplane Flight Dynamic and Automatic Flight Controls, Part 1. Design , Analysis and Research Corporation, 2001.

J. Magni, S. Bennani, and J. Terlouw, Robust Flight Control : A Design Challenge, 1997.
DOI : 10.1007/BFb0113842

Q. Wang and R. F. Stengel, Robust nonlinear flight control of a high-performance aircraft, IEEE Transactions on Control Systems Technology, vol.13, issue.1, pp.15-26, 2005.
DOI : 10.1109/TCST.2004.833651

W. C. John and . Robinson, Block backstepping for nonlinear flight control law design, pp.231-257, 2007.

J. Hauser, S. Sastry, and G. Meyer, Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft, Automatica, vol.28, issue.4, pp.665-679, 1992.
DOI : 10.1016/0005-1098(92)90029-F

L. R. Hunt, R. Su, and G. Meyer, Global transformations of nonlinear systems, IEEE Transactions on Automatic Control, vol.28, issue.1, pp.24-31, 1983.
DOI : 10.1109/TAC.1983.1103137

G. Van-cuong-nguyen and . Damm, Modeling and conditional integrator control of an unmanned aerial vehicle for airlaunch, 2012 American Control Conference (ACC), 2012.
DOI : 10.1109/ACC.2012.6315089