In this paper, a cubic spline guidance law is proposed for intercepting a stationary target at a desired impact angle in surface-to-surface engagement scenarios. An inverse method is used, which represents the altitude as a cubic polynomial of the downrange. The paper addresses many shortcomings of earlier work in this area. In particular, an explicit guidance expression is derived, which makes the guidance law effective and accurate in the presence of disturbances and uncertainties. It is also shown that the guidance command can be obtained using a single cubic spline polynomial even for impact angles greater than and equal to pi/2, While resulting in substantial improvement in terms of lateral acceleration and length of the trajectory. Th...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
This paper proposes a guidance strategy, which caters to both impact angle and impact time terminal ...
In the literature, the impact angle control problem has been addressed mostly against lower speed or...
In this paper, a cubic spline guidance law is proposed for intercepting a stationary target at a des...
In this paper the cubic spline guidance law is presented for intercepting a stationary target at a d...
In this thesis the cubic spline guidance law and its variants are derived. A detailed analysis is c...
Impact angle controlled interception of stationary targets is considered in a surface-to-surface eng...
This paper presents an impact-angle-control guidance law with terminal constraints on the curvature ...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
A polynomial based guidance law dependent on range-to-go, is proposed for interception of a non-mane...
IN MANY advanced guidance applications, it is required to intercept the target from a particular dir...
Guidance laws based on a conventional sliding mode ensures only asymptotic convergence. However, con...
In Many advanced guidance applications [1–5], it is required to intercept the target from a particul...
This thesis deals with development of guidance laws for advanced applications. Two class of guidance...
This paper presents an intercept angle guidance law against moving targets in an environment with se...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
This paper proposes a guidance strategy, which caters to both impact angle and impact time terminal ...
In the literature, the impact angle control problem has been addressed mostly against lower speed or...
In this paper, a cubic spline guidance law is proposed for intercepting a stationary target at a des...
In this paper the cubic spline guidance law is presented for intercepting a stationary target at a d...
In this thesis the cubic spline guidance law and its variants are derived. A detailed analysis is c...
Impact angle controlled interception of stationary targets is considered in a surface-to-surface eng...
This paper presents an impact-angle-control guidance law with terminal constraints on the curvature ...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
A polynomial based guidance law dependent on range-to-go, is proposed for interception of a non-mane...
IN MANY advanced guidance applications, it is required to intercept the target from a particular dir...
Guidance laws based on a conventional sliding mode ensures only asymptotic convergence. However, con...
In Many advanced guidance applications [1–5], it is required to intercept the target from a particul...
This thesis deals with development of guidance laws for advanced applications. Two class of guidance...
This paper presents an intercept angle guidance law against moving targets in an environment with se...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
This paper proposes a guidance strategy, which caters to both impact angle and impact time terminal ...
In the literature, the impact angle control problem has been addressed mostly against lower speed or...