A generalized and unified target state estimation formulation is presented for accurately estimating the states of an airborne target, which can either be nonmaneuvering or undergoing various maneuvers. A nonlinear predictive zero effort miss-based guidance algorithm is also presented here. Extensive high-fidelity six degrees-of-freedom simulation experiments show that near-zero miss distance (i.e., hit-to-kill level performance) can be obtained when these two new techniques are applied together. Moreover, there is a substantial saving in control energy
A nonlinear suboptimal guidance law is presented in this paper for successful interception of ground...
A novel wingman-based estimation and guidance concept is proposed for a sensorless pursuer. The purs...
A three-dimensional strap-down seeker based field of view and impact angle constrained guidance law ...
A generalized and unified target state estimation formulation is presented for accurately estimating...
An extended Kalman filter based generalized state estimation approach is presented in this paper for...
The efficacy of a munition depends on target detection, estimation of its motion, guidance, tracking...
The efficacy of a munition depends on target detection, estimation of its motion, guidance, tracking...
Two different guidance methods are designed for the pre-launch phase in a one-versus-one air combat ...
In this thesis, the problem of intercepting highly manoeuvrable threats using seeker-less intercepto...
An efficient and generalized method of end-game algorithm has been proposed to engage air-borne evad...
This paper addresses the problem of intercepting highly maneuverable threats using seeker-less inter...
An integrated guidance integrated estimation/guidance law is designed for exoatmospheric interceptor...
Approved for public release; distribution unlimited. S,L By using more realistic a priori knowledge ...
In this paper, a novel cooperative and predictive guidance law is proposed to intercept high-speed a...
A generalized approach is presented in this paper for accurately estimating the states of the target...
A nonlinear suboptimal guidance law is presented in this paper for successful interception of ground...
A novel wingman-based estimation and guidance concept is proposed for a sensorless pursuer. The purs...
A three-dimensional strap-down seeker based field of view and impact angle constrained guidance law ...
A generalized and unified target state estimation formulation is presented for accurately estimating...
An extended Kalman filter based generalized state estimation approach is presented in this paper for...
The efficacy of a munition depends on target detection, estimation of its motion, guidance, tracking...
The efficacy of a munition depends on target detection, estimation of its motion, guidance, tracking...
Two different guidance methods are designed for the pre-launch phase in a one-versus-one air combat ...
In this thesis, the problem of intercepting highly manoeuvrable threats using seeker-less intercepto...
An efficient and generalized method of end-game algorithm has been proposed to engage air-borne evad...
This paper addresses the problem of intercepting highly maneuverable threats using seeker-less inter...
An integrated guidance integrated estimation/guidance law is designed for exoatmospheric interceptor...
Approved for public release; distribution unlimited. S,L By using more realistic a priori knowledge ...
In this paper, a novel cooperative and predictive guidance law is proposed to intercept high-speed a...
A generalized approach is presented in this paper for accurately estimating the states of the target...
A nonlinear suboptimal guidance law is presented in this paper for successful interception of ground...
A novel wingman-based estimation and guidance concept is proposed for a sensorless pursuer. The purs...
A three-dimensional strap-down seeker based field of view and impact angle constrained guidance law ...