A New Impact Angle Control Guidance Law to Reduce Sensitivity on Initial Errors
A new homing guidance law to reduce sensitivity on initial heading errors
Impact-Time-Control Guidance with Generalized Proportional Navigation Based on Nonlinear Formulation
Impact-Time-Control Guidance with Generalized Proportional Navigation Based on Nonlinear Formulation
Connections Between Linear and Nonlinear Missile Autopilots via Three-Loop Topology
Connections Between Linear and Nonlinear Missile Autopilots via Three-Loop Topology
Roll-pitch-yaw integrated μ-synthesis for high angle-of-attack missiles