Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 0 of 69 | 100% | 0 of 0 | n/a | 0 | 12 | 0 | 29 | 0 | 12 |
SpacecraftParameters() | 100% | n/a | 0 | 1 | 0 | 7 | 0 | 1 | ||
validate(double) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
setMass(double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
setSolarRadArea(double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
setSolarRadCoeff(double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
setDragArea(double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
setDragCoeff(double) | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | ||
getMass() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getSolarRadArea() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getSolarRadCoeff() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getDragArea() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getDragCoeff() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |