\شماره٪٪۱
Tian, B., Fan, W. and Zong, Q. ``Integrated guidance and control
for reusable launch vehicle in reentry phase''. {\it Nonlinear Dynamics},
{\bf 80}(1), pp. 397-412 (2015).
\شماره٪٪۲
Zhang, L., Wei, C., Wu, R. and et al. ``Adaptive fault-tolerant
control for a VTVL reusable launch vehicle'', {\it Acta Astronautica},
{\bf 159}, pp. 362-370 (2019).
\شماره٪٪۳
Sidipour, H. ``Adaptive integrated nonlinear guidance and control
for an agile device''. M.Sc. Thesis, Sharif University of Technology
(in persion) (1392/2013).
\شماره٪٪۴
Oduntan, G. ``The never ending dispute: Legal theories on
the spatial demarcation boundary plane between airspace and outer
space'', {\it Hertfordshire Law Journal}, {\bf 1}(2), pp. 64-84 (2003).
\شماره٪٪۵
NASA, ``National space transportation system reference: systems
and facilities'', {\bf 1} (June 1988).
\شماره٪٪۶
Lin, C.F., Wang, Q. Spayer, J. L. and et al.
``Integrated estimation, guidance, and control system design
using game theoretic approach'', {\it In 1992 American Control Conference}
(pp. 3220-3224). IEEE (June 1992).
\شماره٪٪۷
Palumbo, N.F., Reardon, B.E. and Blauwkamp, R. ``AIntegrated
guidance and control for homing missiles'', {\it Johns Hopkins APL
Technical Digest}, {\bf 25}(2), pp. 121-139 (2004).
\شماره٪٪۸
Tian, B., Fan, W., Su, R. and et al. ``Real-time trajectory
and attitude coordination control for reusable launch vehicle
in reentry phase'', {\it IEEE Transactions on Industrial Electronics},
{\bf 62}(3), pp. 1639-1650 (2014).
\شماره٪٪۹
Shtessel, Y.B. and Shkolnikov, I.A. ``Integrated guidance
and control of advanced interceptors using second order sliding
modes'', {\it In 42nd IEEE International Conference on Decision and
Control (IEEE Cat. No. 03CH37475)} {\bf 5}, pp. 4587-4592). IEEE
(December 2003).
\شماره٪٪۱۰
Yan, H., Tan, S. and He, Y. ``A small-gain method for integrated
guidance and control in approach and landing phase'', {\it In 2016
35th Chinese Control Conference (CCC)} pp. 10573-10580. IEEE
( July 2016).
\شماره٪٪۱۱
Lai, C., Wang, W., Liu, Z. and et al. ``Three-dimensional integrated
guidance and control for terminal angle constrained attack against
ground maneuvering target'', {\it Proceedings of the Institution of
Mechanical Engineers, Part G: Journal of Aerospace Engineering},
{\bf 233}(7), pp. 2393-2412 (2019).
\شماره٪٪۱۲
Ashrafifar, A. and Jegarkandi, M.F. ``Adaptive fin failures
tolerant integrated guidance and control based on backstepping
sliding mode'', {\it Transactions of the Institute of Measurement
and Control}, {\bf 42}(10), pp. 1823-1833 (2020).
\شماره٪٪۱۳
Lee, H., Wei, C., Cui, N. and et al. ``ntegrated guidance
and control for reusable launch vehicles with actuator failures'',
{\it In 21st AIAA International Space Planes and Hypersonics Technologies
Conference} pp. 2407 (2017).
\شماره٪٪۱۴
Zhang, L., Wei, C., Wu, R. and et al. ``Fixed-time extended
state observer based non-singular fast terminal sliding mode
control for a VTVL reusable launch vehicle'', {\it Aerospace Science
and Technology}, {\bf 82}, pp. 70-79 (2018).
\شماره٪٪۱۵
Wang, J., Cui, N. and Wei, C. ``Optimal rocket landing guidance
using convex optimization and model'', {\it Predictive Control. Journal
Of Guidance, Control, and Dynamics}, {\bf 42}(5), pp. 1078-1092 (2019).
\شماره٪٪۱۶
Tian, B., Fan, W. and Zong, Q. ``Integrated guidance and control
for reusable launch vehicle in reentry phase''. {\it Nonlinear Dynamics},
{\bf 80}(1), pp. 397-412 (2015).
\شماره٪٪۱۷
Recasens, J.J., Chu, Q.P. and Mulder, J.A. ``Robust model
predictive control of a feedback linearized system for a lifting-body
re-entry vehicle'', {\it In AIAA Guidance, Navigation, and Control
Conference and Exhibit} pp. 6147 (August 2005).
)