Re-entry trajectory tracking of reusable launch vehicle using artificial delay based robust guidance law

Author:

Sarkar Rajasree,Mukherjee Joyjit,Patil Deepak,Kar Indra Narayan

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference42 articles.

1. Practical Methods for Optimal Control and Estimation Using Nonlinear Programming;Betts,2010

2. Bollino, Kevin, P., 2006. High-fidelity real-time trajectory optimization for reusable launch vehicles. https://calhoun.nps.edu/handle/10945/10056.

3. Reentry flight controller design using nonlinear dynamic inversion;Da Costa;J. Spacecraft Rock.,2003

4. Integrated finite-time disturbance observer and controller design for reusable launch vehicle in reentry phase;Dong;J. Aerospace Eng.,2016

5. Adaptive-gain multivariable super-twisting sliding mode control for reentry rlv with torque perturbation;Dong;Int. J. Robust Nonlinear Control,2017

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