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TABLE 1: Fixed-parameter tractability of LCS.

in Parameterized Complexity and Biopolymer Sequence Comparison
by Liming Cai, Xiuzhen Huang, Chunmei Liu, Frances Rosamond, Yinglei Song

Table 1: The Fixed-Parameter Complexity of the LCS Problem

in The parameterized complexity of sequence alignment and consensus
by Hans L. Bodlaender, Rodney G. Downey, Michael R. Fellows, Harold T. Wareham 1995
Cited by 30

TABLE 2: Fixed parameter tractability of closest string and closest substring.

in Parameterized Complexity and Biopolymer Sequence Comparison
by Liming Cai, Xiuzhen Huang, Chunmei Liu, Frances Rosamond, Yinglei Song

Table 1: The Fixed-Parameter Complexity of the LCS Problem Alphabet Size j j Problem Parameter Unbounded Fixed

in The Parameterized Complexity of Sequence Alignment and Consensus
by Hans Bodlaender , Rodney G. Downey, Michael R. Fellows, Harold T. Wareham

Table 1: The Fixed-Parameter Complexity of the LCS Problem Alphabet Size j j

in The Parameterized Complexity of Sequence Alignment and Consensus
by Hans L. Bodlaender, Rodney G. Downey, Michael R. Fellows, Harold T. Wareham

Table 2: Physics-based tracking problem: Free and Fixed Parameters

in The University Of Birmingham
by Damien Jade Duff 2006

Table 3: Fixed-parameter values.

in Towards Reducing Thruster-Flexibility Interactions In Space Robots
by E. Martin, E. Papadopoulos, J. Angeles
"... In PAGE 5: ... Parametric Studies and Results Using the describing function method, a parametric study was undertaken to investigate the signin0ccance of key system parameters. The three cases discussed in Section 3 are analyzed using the n0cxed parameter values of Table3 , and the range of parameter values of Table 4, both being based on available space manipulator data 5 . Table 3: Fixed-parameter values.... ..."

Table 1. Fixed-parameter values.

in On the Interaction of Flexible Modes and Ono Thrusters in Space Robotic Systems
by E. Martin, E. Papadopoulos, J. Angeles 1995
Cited by 3

Table 5 Estimates of factor loadings, error variances, and regression coefficients

in Economics of Education Review 23 (2004) 411--430
by Www Elsevier Com, John Schacter A, Yeow Meng Thum B, To Bruner

Table 1: Fixed Parameters No. Parameter De nition 1 D cowl diameter 2

in A Genetic Algorithm for Continuous Design Space Search
by Khaled Rasheed, Haym Hirsh, Andrew Gelsey 1997
"... In PAGE 15: ... Parameter De nition 1 1 initial cone angle 2 2 nal cone angle 3 xd axial location of throat 4 rd radial location of throat 5 xe axial location of end of \constant quot; cross section 6 3 internal cowl lip angle 7 Hej height at end of constant cross section 8 Hfk height at beginning of constant internal cross section Note: All angles measured positive in counter-clockwise direction geometry are not used | the performance of the inlet thus relies solely on the aerodynamic design of the rigid geometry, such as the extent of external and internal compression, con- traction ratio, inlet start throat area, throat location, shock train length, and divergence of subsonic di user. Figure 10 shows the model of the missile geometry which is composed of six xed parame- ters and eight design parameters given in Table1 and Table 2, respectively. The missile inlet is axisymmetric and the coordinates are given in terms of axial (x) and radial (r) positions.... ..."
Cited by 14
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