AIR-BREATHING hypersonic vehicles are intended to be a reliable and cost-effective technology for access to space. In the past few years, a considerable effort has been made …
R Chai, A Tsourdos, A Savvaris, S Chai… - IEEE transactions on …, 2019 - ieeexplore.ieee.org
This brief presents an integrated trajectory planning and attitude control framework for six- degree-of-freedom (6-DOF) hypersonic vehicle (HV) reentry flight. The proposed framework …
N Sarigul-Klijn - Progress in Aerospace Sciences, 2014 - Elsevier
This comprehensive literature survey reviews past and present planetary entry guidance algorithms. The algorithms are categorized based on the vehicle L/D and the planetary …
W Durham, KA Bordignon, R Beck - 2017 - books.google.com
Aircraft Control Allocation An authoritative work on aircraft control allocation by its pioneers Aircraft Control Allocation addresses the problem of allocating redundant flight controls. It …
CE Hall, YB Shtessel - Journal of guidance, control, and dynamics, 2006 - arc.aiaa.org
The nation's goals to replace the aging Space Shuttle fleet and pursue exploration of our solar system and beyond will require more robust, less costly launch vehicles and …
B Tian, W Fan, R Su, Q Zong - IEEE Transactions on Industrial …, 2014 - ieeexplore.ieee.org
The real-time reentry trajectory and attitude coordination control for a reusable launch vehicle (RLV) is a very important and challenging problem. There are many aspects that …
TR Jorris, RG Cobb - Journal of Guidance, Control, and Dynamics, 2009 - arc.aiaa.org
GLOBAL strike and global persistent attack are two of the seven United States Air Force concepts of operations [1]. Various hypersonic and reentry vehicle technologies are being …
B Tian, Q Zong - Acta Astronautica, 2011 - Elsevier
Development of a feasible guidance scheme for reentry vehicles is a challenge because of its significant nonlinearity and multi-constraints. A method for the implementation of three …
A new method of controlling a flapping-wing micro air vehicle by varying the velocity profiles of the wing strokes is presented in this manuscript. An exhaustive theoretical analysis along …