Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads

By P. Menon, G. Sweriduk, E. Ohlmeyer, D. S. Malyevac. 2004

186 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/d4796343bdd4093607b697a059b5ed2da05488e6

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Jinzhi Wang
2. Xianghua Wang

In Computational Mechanics

1. Jinzhi Wang
2. Xianghua Wang

Citations in the corpus

• Partial Integrated Missile Guidance and Control with Finite Time Convergence (2013, methodology): “Up to now, various control methods for homing missiles have been incorporated with IGC, for example, backstepping [16], θ-D method [17], subspace stabilization [18], linear optimal control theory [19], feedback linearization [20], game theory [21], and the state-dependent Riccatti equation (SDRE) [2”