Stochastic optimal control guidance law with bounded acceleration
Stochastic optimal control guidance law with bounded acceleration
- New search for: Hexner, G.
- New search for: Shima, T.
- New search for: Hexner, G.
- New search for: Shima, T.
A novel stochastic optimal control guidance law is presented for a missile with bounded acceleration. The nonlinear optimal guidance law (NOGL) is obtained by numerically solving the stochastic optimization problem. Since the certainty equivalence principle is not valid in the investigated problem, the resulting NOGL depends on the conditional probability density function of the estimated states. It is shown that the NOGL is also nonlinear in the estimated zero effort miss distance, and that the probability density function of the miss distance is non-Gaussian. The dependence of the new guidance law on the acceleration limit is investigated and it is shown that only for an extremely large acceleration limit does the proposed guidance law degenerate to the classical optimal linear one
Document information
Stochastic optimal control guidance law with bounded acceleration
IEEE Transactions on Aerospace and Electronic Systems ; 43 , 1 ; 71-78
2007-01-01
1086119 byte
Article (Journal)
Electronic Resource
English
Similar titles
Stochastic Optimal Control Guidance Law with Bounded Acceleration
| Online Contents | 2007
Practical Stochastic Optimal Guidance Law for Bounded Acceleration Missiles
| Online Contents | 2011
Model Matched Stochastic Guidance Law for a Bounded Acceleration Missile
| British Library Conference Proceedings | 2009
LQC guidance law with bounded acceleration command
| IEEE | 2008