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Guidance impulse algorithms for air bomb control

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Treść / Zawartość
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In this paper, some results of research concerning the development of guidance of bombs were presented. The paper presents conceptions of an impulse (gasodynamic) control system, the measurement unit based on IMU/GPS signals and control algorithms based on predicted trajectories. The presented results of simulation research are based on the numerical model of the bomb and real signals from measurement devices.
Rocznik
Strony
825--833
Opis fizyczny
Bibliogr. 12 poz., rys., tab.
Twórcy
  • Faculty of Power and Aeronautical Engineering, Warsaw University of Technology, 24 Nowowiejska St., 00-665 Warszawa, Poland
Bibliografia
  • [1] H. Klotz and C. Derbak, GPS- aided Navigation and UnaidedNavigation on the Joint Direct Attack Munitions, IEEE, London, 1998.
  • [2] R. Kostrow, M. Makuszewski, and M. Studencki, Rockets andRocket Artillery of the Army, Bellona, Warszawa, 2001, (in Polish).
  • [3] R. Glebocki and R. Vogt, “Guidance system of smart mortar missile”, The Archive Mechanical Engineering LIV (1), 47-63 (2007).
  • [4] R. Głębocki and M. Żugaj, “Gasodynamic control system for INS guided bomb”, 47th AIAA Aerospace Sciences Meetingand Exhibit 1, CD-ROM (2009).
  • [5] Z. Dziopa, I. Krzysztofik, and Z. Koruba “An analysis of the dynamics of a launcher-missile system on a moveable base”, Bull. Pol. Ac.: Tech. 58, 645-650 (2010).
  • [6] J. Gacek, External Ballistics, WAT Publishing House, Warszawa, 1999, (in Polish).
  • [7] Z. Koruba and J. Osiecki, Construction, Dynamics and Navigationof Selected Precise Destruction Weapons, Kielce University of Technology Publishing House, Kielce, 2006.
  • [8] Z. Koruba, I. Krzysztofik, and Z. Dziopa “An analysis of the gyroscope dynamics of an anti-aircraft missile launched from a mobile platform”, Bull. Pol. Ac.: Tech. 58, 651-656 (2010).
  • [9] R. Głębocki, R. Vogt, and M. Żugaj, “Smart mortar missile attitude detection based on the algorithm that takes advantage of the artificial neural networks”, AIAA Guidance Navigationand Control Conference and Exhibit 1, CD-ROM (2006).
  • [10] W.H. Chen, “Nonlinear disturbance observer-enhanced dynamic inversion control of missiles”, J. Guidance, Control, andDynamics 26, 161-166 (2003).
  • [11] P.A. Iglesian and T.J. Urban, “Loop shaping design for missile autopilot”, J. Guidance, Control, and Dynamics 23, 516-525 (2000).
  • [12] T. Kaczorek, “Stability of continuous-discrete linear systems described by the general model”, Bull. Pol. Ac.: Tech. 59, 189-193 (2011).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPG8-0096-0047
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