A validation method relating to the detection of a crossing of the Krmn line by a portable object (2) carried on board a rocket and incorporating a detection device including an acceleration sensor (8) capable of measuring accelerations of the portable object and an electronic unit for processing the acceleration measurements made so as to detect a crossing of the Krmn line by the portable object. The method calculates a confidence index, relating to measurements made by the portable object for a variable which is a function of forces exerted on this portable object, and checks whether a condition given for the confidence index is met. Also, a portable object, in particular a watch, designed to be able to implement a method for detecting a crossing of the Krmn line and the validation method of the invention.

Provided is a sensor apparatus that includes a substrate, one or more first IMU sensors, and one or more second IMU sensors. The substrate has a first surface and a second surface opposite to the first surface. The one or more first IMU sensors are arranged on the first surface. The one or more second IMU sensors are arranged on the second surface. By arranging the IMU sensors on both the first surface and the second surface, it is possible to reduce the size of the apparatus and to suppress a deformation of the substrate due to heat. This makes it possible to realize a highly accurate measurement based on a detection result (sensing result) of a plurality of IMU sensors.

A MEMS inertial sensor device, method of operation, and fabrication process are described with a MEMS inertial sensor, drive actuation unit, drive measurement unit, and PLL circuit coupled together in operational engagement, where the MEMS inertial sensor includes a substrate, a proof mass positioned in spaced apart relationship above the substrate, a proof mass suspension member connected on a first end to the proof mass and connected on a second end to an anchor fixed to the substrate to enable the proof mass to laterally oscillate over the surface of the substrate, and a compliant stop structure positioned in relation to the proof mass suspension member to physically engage with lateral oscillating movement of the proof mass suspension member past a desired stroke travel distance without physically preventing lateral oscillating movement of the proof mass, thereby stiffening a spring stiffness measure of the proof mass suspension member.

Inertial sensors with a bulk substrate proof mass are disclosed herein. In certain embodiments, an inertial sensor includes a bulk substrate and a bulk substrate proof mass formed from the bulk substrate. Additionally, the inertial sensor further includes a sensing structure that detects a relative motion between the bulk substrate and the bulk substrate proof mass. Accordingly, a portion of the bulk substrate is used to form the proof mass, which moves in a cavity relative to another portion of the bulk substrate that is fixed. Such an inertial sensor can provide a number of benefits including, for example, lower stiction risk, stiffer tethering, and/or lower Brownian noise.