• DocumentCode
    486216
  • Title

    Linearization of Digital Derived Rate Algorithm for Use in Linear Stability Analysis

  • Author

    Graham, Ronald E. ; Porada, Theodore W.

  • Author_Institution
    NASA-Lewis Research Center, Cleveland, OH
  • fYear
    1985
  • fDate
    19-21 June 1985
  • Firstpage
    139
  • Lastpage
    143
  • Abstract
    The digital derived rate (DDR) algorithm is used to calculate the rate of rotation of the Centaur upper-stage rocket. The DDR is a highly nonlinear algorithm, and classical linear stability analysis of the spacecraft cannot be performed without linearization. The performance of this rate algorithm is characterized by a gain and phase curve that drop off at the same frequency. This characteristic is useful in many applications. This paper deals with the investigation of a linearization technique for the DDR algorithm. The linearization method is described. Examples of the results of the linearization technique are illustrated, and the effects of linearization are described. A linear digital filter may be used as a substitute for the DDR in classical linear stability analyses, while the DDR itself may be used in time response analysis.
  • Keywords
    Engines; Frequency response; Linearization techniques; Pi control; Proportional control; Quantization; Sampling methods; Stability analysis; Time factors; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1985
  • Conference_Location
    Boston, MA, USA
  • Type

    conf

  • Filename
    4788594