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  • SPACECRAFT DESIGN, TESTING AND PERFORMANCE  (2)
  • tissue culture  (1)
  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Plant cell, tissue and organ culture 9 (1987), S. 29-35 
    ISSN: 1573-5044
    Keywords: tissue culture ; micropropagation ; rhizome tip ; Alstroemeria
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology
    Notes: Abstract Plantlets were regenerated from Alstroemeria ‘Alsaan’ rhizome tips cultured in vitro on solid and liquid media based on Murashige and Skoog salt formulation. The quality of the cultures was superior when intact rather than longitudinally sliced rhizome tips were used as explants and when a temperature of 8°C rather than 22°C was used at the initiation stage. More roots were produced on rhizome tips containing a rhizome apical meristem than on rhizome sections lacking such a meristem. Most (90%) of the rooted plantlets were successfully acclimatized and developed into true-to-type flowering plants.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-06-28
    Description: A decoupling and pole-placement technique has been developed for the Annular Suspension and Pointing System (ASPS) of the Space Shuttle which uses bandwidths as performance criteria. The dynamics of the continuous-data ASPS allows the three degrees of freedom to be totally decoupled by state feedback through constant gains, so that the bandwidth of each degree of freedom can be independently specified without interaction. Although it is found that the digital ASPS cannot be completely decoupled, the bandwidth requirements are satisfied by pole placement and a trial-and-error method based on approximate decoupling.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Computers and Electrical Engineering; 7; Dec. 198
    Format: text
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  • 3
    Publication Date: 2019-07-13
    Description: The Annular Suspension and Pointing System (ASPS) is a payload auxiliary pointing device of the Space Shuttle. The ASPS is comprised of two major subassemblies, a vernier and a coarse pointing subsystem. The three functions provided by the ASPS are related to the pointing of the payload, centering the payload in the magnetic actuator assembly, and tracking the payload mounting plate and shuttle motions by the coarse gimbals. The equations of motion of a simplified planar model of the ASPS are derived. Attention is given to a state diagram of the dynamics of the ASPS with position-plus-rate controller, the nonlinear spring characteristic for the wire-cable torque of the ASPS, the design of the analog ASPS through decoupling and pole placement, and the time response of different components of the continuous control system.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 79-0398 , American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting; Jan 15, 1979 - Jan 17, 1979; New Orleans, LA
    Format: text
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