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eess.SY2026

Optimal Guidance with Terminal Intercept-Angle Constraints and Acceleration Bounds

Yoav Azaryahu, Vitaly Shaferman

Terminal intercept-angle control against a maneuvering target can substantially increase the required missile acceleration, potentially leading to saturation and interception failu…

eess.SY2026

Optimal Ground-to-Air Interception with Time-Varying Acceleration Bounds

Or Nahum, Vitaly Shaferman

This paper proposes novel optimal-control-based guidance laws for ground-to-air missiles with time-varying acceleration bounds. In such engagements, as the missile climbs in altitu…

eess.SY2026

Low-Thrust Orbital Differential Games with Speed Constraint Enforcement Using Cost Weighting

Yahli Drucker, Vitaly Shaferman

This paper considers the problem of a low-thrust spacecraft pursuit-evasion differential game with an arbitrary terminal relative speed constraint. It addresses the terminal phase…

eess.SY2026

Optimal Powered Descent Guidance with Pyramid-Shaped Approach-Angle Constraints

Revital Frenkel, Vitaly Shaferman

In this paper, a novel optimal soft-landing guidance law with inequality approach-angle path constraints is analytically derived. The proposed guidance law prevents ground collisio…

eess.SY2026

Optimal Bounded Thrust Powered Descent with Analytical Ground-Collision Avoidance

Or Nataf, Vitaly Shaferman

The paper proposes a new approach to address the bounded-thrust powered-descent problem while ensuring ground-collision avoidance. A time-dependent polynomial approximation of the…