Abstract: A system may include a plurality of inhalers, where each inhaler comprising medicament, a processor, memory, and a transmitter, multiple processing modules that may reside at least partially on a user device, a digital health platform (DHP) that is configured to receive and aggregate inhaler data from inhalers that are associated with a plurality of different users and a plurality of different medicament types. The DHP may be configured to train a machine learning algorithm using training data via a supervised or an unsupervised learning method, wherein the training data comprises the time and the one or more inhalation parameters associated with each of the plurality of usage events. The DHP also configured to generate a compliance score, a future compliance score, and/or a risk score using the trained machine learning algorithm, and cause a display device to generate a notification indicating the score for the user.

Abstract: The present technical solution solves a problem of keeping a given direction by use of an element stabilized in a given plane of inertial space, irrespective of disturbing torques, precessions of gyroscopes, and turns of a movable object in the given plane of inertial space when the current technical solution is used on the movable object. This solution is based on forcing precessions of two one-axis gyrostabilizers in opposite directions. The gyrostabilizers are connected with each other by a connection unit comprising a stabilized element. Since in the present solution low precision gyroscopes can be used, then the proposed solution can be implemented in a small-size version.

Abstract: The technical solution provided can be implemented with the help of two miniature vessels and even one miniature vessel filled with the flowing media. It is based on determining the pressures difference in particular points, wherein the pressures caused by the cross accelerations and other disturbance factors are considered to be equal, and the ones caused by the acceleration determined are considered to be different. The present solution enables one to determine the acceleration with higher accuracy even with big tilting (practically up to 360°) of the platform, in particular, on the body of a moving object, the acceleration whereof is determined.

Abstract: The present technical solution provided allows it to determine true meridian of any movable object. This solution is based on determining true meridian by zero value of linear acceleration induced created by changing the projection of the vector of linear velocity, caused by rotating any heavenly body, in particular, the terrestrial globe. The determination is implemented in compact variant only by the devices located on the movable object without any necessity of using induced radiations, quickly and accurately without any necessity of knowing the coordinates of location and the speed of movement irrespective of weather conditions, transverse accelerations, temperature changes and external magnetic fields influence.

Abstract: The present technical solution for determining linear acceleration, the vector whereof is considered to be at a tangent to a trajectory of movement of a moving object, is based on determining new differences of accelerations. It is considered to be the basis for efficient, accurate, with the threshold of sensitivity equal to zero in small-size option solving the tasks of autonomous navigation, piloting, stabilization and etc. Said solution is irrespective of disturbance factors, in particular, cross-axis and centrifugal accelerations, vibrations, temperature and others, and can be used without any gyroscopes.

Abstract: The technical solution provided enables it to determine true meridian of an unmovable object on the Earth, and when moving at constant velocity true track angle. This solution is based on fixation of true meridian by zero value of linear acceleration with induced rotating points of determining pressure around the vertical. Said determinations are implemented quickly and accurately, irrespective of the disturbing factors influence, in particular, electromagnetic and magnetic fields, weather conditions, vibrations, cross accelerations, temperature and others.

Abstract: The present technical solution provided for the autonomous determination of wind speed vector is intended for the accurate determination of wind speed vector as well sea current, only by the means located in a moving object without applying any radiations and gyroscopes, and also without applying any sources of information and reference marks on the Earth and other heavenly bodies. Such determination is proposed for the first time and is if paramount importance for the navigation purposes, in particular, for the determination of ground speed vector of a moving object and also for meteorology. This solution is based on the determination and transformation of the horizontal projections of linear acceleration vector of the moving object by means of the sensors of acceleration developed by the authors previously with applying the value of the course of a moving object and its speeds.

Abstract: The present technical solution provided is intended for the accurate determination of angle of drift only by the means located inside the moving object, without applying any radiations and gyroscopes as well as without using any sources of information and orientation on the Earth and on any other heavenly bodies. The determination of such kind is provided for the first time and is considered to be of paramount importance for the navigational and meteorological purposes. The present solution is based on the determination of the horizontal projections of the linear acceleration vector by means of the sensors of said acceleration, they being developed by the authors earlier.

Abstract: The present technical solution for determining linear acceleration, the vector whereof is considered to be at a tangent to a trajectory of movement of a moving object, is based on determining new differences of accelerations. It is considered to be the basis for efficient, accurate, with the threshold of sensitivity equal to zero in small-size option solving the tasks of autonomous navigation, piloting, stabilization and etc. Said solution is irrespective of disturbance factors, in particular, cross-axis and centrifugal accelerations, vibrations, temperature and others, and can be used without any gyroscopes.

Abstract: The technical solution provided of determining the vertical on the moving object is based on bringing the difference of apparent and horizontal accelerations to zero. It enables one to solve the tasks of determining the parameters of movement with the threshold of sensitivity equal to zero with efficiency and accuracy, and in small-size version (compactness). This solution can be used without any gyroscopes, and be implemented irrespective of disturbance factors influence, in particular, transverse and centrifugal accelerations, vibrations, temperatures and others.

Abstract: The present technical solution provided allows it to determine true meridian of any movable object. This solution is based on determining true meridian by zero value of linear acceleration induced created by changing the projection of the vector of linear velocity, caused by rotating any heavenly body, in particular, the terrestrial globe. The determination is implemented in compact variant only by the devices located on the movable object without any necessity of using induced radiations, quickly and accurately without any necessity of knowing the coordinates of location and the speed of movement irrespective of weather conditions, transverse accelerations, temperature changes and external magnetic fields influence.

Abstract: The present technical solution provided allows it to meet the problem of keeping the direction given by the use of the stabilized element in the plane of the inertial space, irrespective of acting harmful torques, precessions of gyroscopes and turns in that plain of the movable object whereon the solution is used. This solution is based on forced creation of those precessions of two one-axis gyrostabilizers towards the opposite sides, connected with each other by the connection unit comprising the stabilized element. Since in the present solution use can be made of the gyroscope of low accuracy, then the solution provided can be implemented in the small-size version.

Abstract: The technical solution provided enables it to determine true meridian of an unmovable object on the Earth, and when moving at constant velocity true track angle. This solution is based on fixation of true meridian by zero value of linear acceleration with induced rotating points of determining pressure around the vertical. Said determinations are implemented quickly and accurately, irrespective of the disturbing factors influence, in particular, electromagnetic and magnetic fields, weather conditions, vibrations, cross accelerations, temperature and others.

Abstract: The technical solution provided can be implemented with the help of two miniature vessels and even one miniature vessel filled with the flowing media. It is based on determining the pressures difference in particular points, wherein the pressures caused by the cross accelerations and other disturbance factors are considered to be equal, and the ones caused by the acceleration determined are considered to be different. The present solution enables one to determine the acceleration with higher accuracy even with big tilting (practically up to 360°) of the platform, in particular, on the body of a moving object, the acceleration whereof is determined.

Abstract: The technical solution provided relating to the undisturbed, accurate, fast determination on the moving object of the gravitational vertical is based on the determination of the signals of the accelerations difference supplied to the actuating mechanism holding the platform, whereon the said accelerations are determined, in the horizontal position. The present solution can be implemented with the gyroscope (including not high accuracy) and even without the latter. As the platform use can be made of the body of the moving object, in particular, an aircraft.

Abstract: The method for determining the vertical acceleration is based on the determination of the pressures difference in particular points, wherein the pressures created by the vertical acceleration are considered to be different and, the ones created by the cross accelerations are considered to be equal. According to the method there are provided the miniature devices intended for realizing the said solution. The two of these devices comprise two-vessel and one-vessel ones. One of the two-vessel devices and one-vessel device have only one sensitive element of pressure, which is considered to eliminate any harmful influence of the parameters spread of the sensitive elements of pressure. The pressure sensors of the said devices are to be switched to the differential scheme, at the output thereof the signal of the vertical acceleration is taken. The technical solution in hand is expected to eliminate any harmful influence of the disturbing factors, particularly, cross accelerations.

Abstract: The device for measuring horizontal acceleration consisting of two similar hermetically sealed vessels containing liquid and provided with the pressure sensors connected to the differential scheme. The determination of the accelerations is done in terms of these sensors signals difference, which measuring the pressure in particular points. In these very points the pressures created by the vertical acceleration are equal in terms of each other, the ones created by the horizontal acceleration are different.

Abstract: The device for measuring horizontal acceleration consisting of two similar hermetically sealed vessels containing liquid and provided with the pressure sensors connected to the differential scheme. The determination of the accelerations is done in terms of these sensors signals difference, which measuring the pressure in particular points. In these very points the pressures created by the vertical acceleration are equal in terms of each other, the ones created by the horizontal acceleration are different.