Coverage Report for FCC_Sys_New_v2

Table of Contents

  1. Analysis Information
  2. Tests
  3. Summary
  4. Details

Analysis Information

Model Information

  Model version   1.94
  Author   bpotter
  Last saved   Thu Oct 15 21:31:31 2020

Simulation Optimization Options

  Default parameter behavior   inlined
  Block reduction   forced off
  Conditional branch optimization   on

Coverage Options

  Analyzed model   FCC_Sys_New_v2
  Logic block short circuiting   off

Tests

Test# Started execution Ended execution Description
Test 1 15-Oct-2020 23:29:16 15-Oct-2020 23:29:34 This model represents a flight control system for a helicopter that controls pitch attitude, roll attitude and yaw rate based on pilot inputs from the cyclic and pedals. The flight control computer also closes the loop on three hydrualic actuators and has sensor inputs from three Attitude/Heading Reference Systems.

Summary

Model Hierarchy/Complexity Test 1  
Execution  
1. FCC_Sys_New_v2   100%
   
 

Details

1. Model "FCC_Sys_New_v2"


Metric Coverage (this object) Coverage (inc. descendants)
Execution NA 100% (1/1) objective outcomes

   Full Coverage

Model Object Metric
ModelReference block "FCC_New" Execution