A new guidance law with both impact time and impact angle constraints is proposed in this
paper. We first simplify missile dynamics under small heading error approximation, and …

MAINTAINING seeker lock on to the target is critical for the success of any missile
engagement. Imposing a terminal impact angle constraint may result in curved missile …

WHEN a pursuer for some reason modifies its otherwise direct course toward a target, two
key quantities that become significantly influenced are the impact time and the impact angle …

Nomenclature a= missile lateral acceleration, m∕ s2 amax= limit of missile lateral
acceleration, m∕ s2 N= proportional-navigation gain r= range between missile and target …

Aiming at the terminal impact-angle constraint in the interception of large maneuvering
targets, this paper proposes a three-dimensional (3D) interception guidance law combined …

In this paper, an impact angle control guidance law, which considers simultaneously the
impact angle and seeker's look angle constraints, is proposed for a constant speed missile …

OWING to the stringent performance requirements, guidance and control design for tactical
missiles is still an area of active research. In modern missile guidance, the concept of …

This paper presents an impact angle control guidance law that confines the missile look
angle during homing in order to not exceed a seeker's field-of-view limit. A sliding surface …

In this article, a practical three-dimensional (3-D) guidance is designed to achieve trajectory
constrained flight, ie, arriving at the destination with desired approach angles under limited …

This paper proposes a guidance law that achieves the desired terminal impact time without
violating a seeker's field-of-view (FOV) limits. In order to derive the guidance law, kinematic …