مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Verion

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

video

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

sound

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Version

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

View:

282
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Download:

0
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Cites:

Information Journal Paper

Title

Simulation and Performance Investigation of a Typical Guidance System with Suitable Modeling of the Guidance System Elements and its Sensitivity with Respect to Aerodynamic Coefficients

Pages

  235-249

Abstract

 The Guidance commands are mostly generated by determining of the line of sight (LOS) angle. Among the existed Guidance laws, proportional navigation (PN) is the most widely used algorithm. In this way, the differentiation of the LOS angle is required. Then the LOS rate are usually computed by numerical differentiation of the LOS angle. The LOS rate can be directly measured by an embedded internal seeker which it would be a differential free technique. Nowadays, in practical, guidance algorithms equipped with a seeker have been interested. Such a guidance loop includes some subsystems like vehicle dynamics, the type of flight path and also navigation sensors. Each subsystems may have some parameters as well as aerodynamic coeficients. Thererfore the Guidance System Performance would be affected by changing in these parameters. In this paper, in a typical vehicle equipped with a seeker, the guidance system efficiency would be numerically investigated in terms of the aerodynamic coeficients change.

Cites

  • No record.
  • References

  • No record.
  • Cite

    APA: Copy

    GHAFFARI, V., MOHAMMADKHANI, H., & HEYDARI, K.. (2018). Simulation and Performance Investigation of a Typical Guidance System with Suitable Modeling of the Guidance System Elements and its Sensitivity with Respect to Aerodynamic Coefficients. JOURNAL OF SOLID AND FLUID MECHANICS, 8(2 ), 235-249. SID. https://sid.ir/paper/393510/en

    Vancouver: Copy

    GHAFFARI V., MOHAMMADKHANI H., HEYDARI K.. Simulation and Performance Investigation of a Typical Guidance System with Suitable Modeling of the Guidance System Elements and its Sensitivity with Respect to Aerodynamic Coefficients. JOURNAL OF SOLID AND FLUID MECHANICS[Internet]. 2018;8(2 ):235-249. Available from: https://sid.ir/paper/393510/en

    IEEE: Copy

    V. GHAFFARI, H. MOHAMMADKHANI, and K. HEYDARI, “Simulation and Performance Investigation of a Typical Guidance System with Suitable Modeling of the Guidance System Elements and its Sensitivity with Respect to Aerodynamic Coefficients,” JOURNAL OF SOLID AND FLUID MECHANICS, vol. 8, no. 2 , pp. 235–249, 2018, [Online]. Available: https://sid.ir/paper/393510/en

    Related Journal Papers

    Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    Move to top
    telegram sharing button
    whatsapp sharing button
    linkedin sharing button
    twitter sharing button
    email sharing button
    email sharing button
    email sharing button
    sharethis sharing button