A helicopter is susceptible to a rolling tendency,called dynamic rollover, when close to the ground,especially when taking off or landing.For dynamic rollover to occur, some factor has to firstcause the helicopter to roll or pivot around a skid, orlanding gear wheel, until its critical rollover angle isreached. Then, beyond this point, main rotor thrust continuesthe roll and recovery is impossible. If the criticalrollover angle is exceeded, the helicopter rolls on itsside regardless of the cyclic control corrections made.[1] [2]
Dynamic rollover begins when the helicopter starts topivot around its skid or wheel. This can occur for avariety of reasons, including the failure to remove atiedown or skid securing device, or if the skid or wheelcontacts a fixed object while hovering sideward, or ifthe gear is stuck in ice, soft asphalt, or mud. Dynamicrollover may also occur if the pilot does not use the properlanding or takeoff technique or while performing slopeoperations. Whatever the cause, if the gear or skidbecomes a pivot point, dynamic rollover is possible ifthe pilot does not use the proper corrective technique.
Once started, dynamic rollover cannot be stopped byapplication of opposite cyclic control alone. For example, ifthe right skid contacts an object and becomes thepivot point while the helicopter starts rolling to theright, even with full left cyclic applied the main rotorthrust vector and its moment follows the aircraft as itcontinues rolling to the right. Quickly applying downcollective is the most effective way to stop dynamicrollover from developing. Dynamic rollover can occurin both skid and wheel equipped helicopters, and alltypes of rotor systems.
Static Rollover is a rolling action when the helicopter blades are not in rotation. When the rotor blades stop, the helicopter has the same principles of any other object and will roll if the static rollover critical angle is exceeded. Each helicopter has its own critical angle; this is a byproduct of its center-of-gravity.
A rolling object has a pivot point and an imaginary line extending upward from the pivot point; as the object rolls around the pivot point, the center of gravity moves closer to the pivot line. Only upon passing the pivot line will the object roll to the corresponding adjacent side of the base.
The static rollover critical angle can be determined by measuring the angle between level ground and an imaginary line drawn from skid to skid, when the helicopter's center of gravity is located on the upward pivot line.[3] [4]
Static rollover also pertains to automobiles. In the study of roll stability of vehicles, the static rollover threshold is a key measure. It is expressed as a lateral acceleration in gravitational units. In reality, rollovers are dynamic events; however, there is a strong relationship between roll stability and occurrences of rollover in accidents.[5]