Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 0 of 70 | 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 |