Abstract
Guidance and control laws design for a switched flight system with discontinuous actuators is dealt with in this paper. Firstly, a missile equipped with discontinuous side jets is introduced. Secondly, the side-jet missile is modeled with an impulsive switched system. Thirdly, a sliding mode control-based discontinuous guidance law is proposed to generate guidance commands, which are suitable for on–off side jets. And a logic-based switching law for turning on the side jets is also submitted. Fourthly, by transforming the discontinuous actuators equivalently and formulating an extended state space equation, a tracking control law is indicated to track the guidance command. Finally, simulations and comparisons are made to demonstrate the proposed algorithms.
Original language | English |
---|---|
Pages (from-to) | 829-846 |
Number of pages | 18 |
Journal | Optimal Control Applications and Methods |
Volume | 38 |
Issue number | 5 |
DOIs | |
Publication status | Published - 1 Sept 2017 |
Externally published | Yes |
Keywords
- discontinuous actuators
- guidance law
- switched system
- switching law
- tracking control