Control allocation—A survey

TA Johansen, TI Fossen - Automatica, 2013 - Elsevier
The control algorithm hierarchy of motion control for over-actuated mechanical systems with
a redundant set of effectors and actuators commonly includes three levels. First, a high-level …

Nonlinear robust adaptive control of flexible air-breathing hypersonic vehicles

L Fiorentini, A Serrani, MA Bolender… - Journal of guidance …, 2009 - arc.aiaa.org
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 …

Six-DOF spacecraft optimal trajectory planning and real-time attitude control: a deep neural network-based approach

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 …

Survey of planetary entry guidance algorithms

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 …

[图书][B] Aircraft control allocation

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 …

Sliding mode disturbance observer-based control for a reusable launch vehicle

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 …

Real-time trajectory and attitude coordination control for reusable launch vehicle in reentry phase

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 …

Three-dimensional trajectory optimization satisfying waypoint and no-fly zone constraints

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 …

Optimal guidance for reentry vehicles based on indirect Legendre pseudospectral method

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 …

Wingbeat shape modulation for flapping-wing micro-air-vehicle control during hover

DB Doman, MW Oppenheimer… - Journal of guidance …, 2010 - arc.aiaa.org
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 …