Robust gain-scheduled autopilot design with anti-windup compensation for a guided projectile
Author:
Publisher
Springer Science and Business Media LLC
Subject
Aerospace Engineering,Transportation
Link
https://link.springer.com/content/pdf/10.1007/s13272-023-00668-9.pdf
Reference39 articles.
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2. Burchett, B., Peterson, A., Costello, M.: Prediction of swerving motion of a dual-spin projectile with lateral pulse jets in atmospheric flight. Math. Comput. Model. 35(7–8), 821–834 (2002). https://doi.org/10.1016/S0895-7177(02)00053-5
3. Hahn, P.V., Frederick, R.A., Slegers, N.: Predictive guidance of a projectile for hit-to-kill interception. IEEE Trans. Control Syst. Technol. 17(4), 745–755 (2009). https://doi.org/10.1109/tcst.2008.2004440
4. Frost, G., Costello, M.: Control authority of a projectile equipped with an internal unbalanced part. J. Dyn. Syst. Meas. Contr. 128(4), 1005 (2006). https://doi.org/10.1115/1.2363205
5. Rogers, J., Costello, M.: A variable stability projectile using an internal moving mass. Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. 223(7), 927–938 (2009). https://doi.org/10.1243/09544100jaero509
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