Linear Quadratic Guidance Laws for Imposing a Terminal Intercept Angle
- 1 September 2008
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 31 (5), 1400-1412
- https://doi.org/10.2514/1.32836
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Time-to-go weighted optimal guidance with impact angle constraintsIEEE Transactions on Control Systems Technology, 2006
- Sliding-Mode Control for Integrated Missile Autopilot GuidanceJournal of Guidance, Control, and Dynamics, 2006
- Optimal Guidance Laws with Terminal Impact Angle ConstraintJournal of Guidance, Control, and Dynamics, 2005
- Impact angle control for planar engagementsIEEE Transactions on Aerospace and Electronic Systems, 1999
- Biased PNG law for impact with angular constraintIEEE Transactions on Aerospace and Electronic Systems, 1998
- Optimal planar interception with terminal constraintsJournal of Guidance, Control, and Dynamics, 1995
- Terminal Guidance for Impact Attitude Angle Constrained Flight TrajectoriesIEEE Transactions on Aerospace and Electronic Systems, 1973
- Optimum intercept laws for accelerating targets.AIAA Journal, 1968