In this paper, we present a novel systematic approach for the autopilot design of STT missiles. First, the nonlinear model of a STT missile is partially ...
We present a systematic approach for the autopilot design of skid-to-turn (STT) missiles. First, the nonlinear model of a STT missile is partially linearized ...
This paper presents a new approach to acceleration control of. STT (Skid-To-Turn) missiles. In the design and stability analysis of our autopilot, we assume ...
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This paper describes the design and implementation of a three-axis acceleration control autopilot for an asymmetric tail-controlled, skid-to-turn tactical ...
Apr 25, 2024 · Design of a STT missile autopilot using functional inversion and LMI approach. ... with time-varying delays in state. Autom. 35(9): 1587 ...
Feb 14, 2019 · This work presents a novel robust control design approach for missile longitudinal autopilot under multiple disturbances and uncertainties.
This paper presents a procedure of a Sum-Of-Squares (SOS) based autopilot design for a Skid-To-Turn (STT) missile. In particular, we consider a nonlinear ...
Abstract. This work presents a novel robust control design approach for missile longitudinal autopilot under multiple disturbances and uncertainties.
This paper considers integrated guidance and control system with input saturation for homing missiles based on the three channels independence design idea.
Missile autopilot design via functional inversion and time-scaled transformation · Robust feedback linearization approach to autopilot design · Nonlinear flight ...
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