Control of Impact Time with Increased Robustness via Feedback Linearization
- 1 July 2016
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 39 (7), 1682-1689
- https://doi.org/10.2514/1.g001719
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
- Lyapunov-Based Guidance Law for Impact Time Control and Simultaneous ArrivalJournal of Guidance, Control, and Dynamics, 2016
- Impact time control guidance law with field of view constraintAerospace Science and Technology, 2014
- Design of Time-constrained Guidance Laws via Virtual Leader ApproachChinese Journal of Aeronautics, 2010
- Homing Guidance Law for Cooperative Attack of Multiple MissilesJournal of Guidance, Control, and Dynamics, 2010
- Cooperative Guidance for Multimissile Salvo AttackChinese Journal of Aeronautics, 2008
- Impact-time-control guidance law for anti-ship missilesIEEE Transactions on Control Systems Technology, 2006
- Guidance Algorithm Design: A Nonlinear Inverse ApproachJournal of Guidance, Control, and Dynamics, 1998
- Guidance of a homing missile via nonlinear geometric control methodsJournal of Guidance, Control, and Dynamics, 1995
- Ideal proportional navigationJournal of Guidance, Control, and Dynamics, 1992
- Design of a CLOS guidance law via feedback linearizationIEEE Transactions on Aerospace and Electronic Systems, 1992