Patent RU-2765674-C1 (RU)
Title: Method for standardising the flight load of a helicopter pilot when performing the "aerobatics complex" exercise
Inventor: Koronkov Sergej Olegovich
IPC: A61B5/00
Filed: 2021-01-27
Granted: 2022-02-01
Abstract: FIELD: educating. 
     SUBSTANCE: invention relates to methods for professional training of helicopter pilots. Proposed is a method for standardising the professional load of a helicopter pilot when performing the "Speed acceleration" exercise, consisting in the fact that no later than 10 minutes before the beginning of simulator training, the pulse rate and breathing rate of the pilot are recorded at least three times, the recorded values are averaged by calculating the arithmetic average values thereof, and said values are taken as background values of the pulse rate (x1f) and breathing rate (x2f); then seven exercises are performed in a clear sequence: 1) the "speed acceleration" exercise, before the beginning whereof, the optimal trajectory of the "acceleration speed" exercise is calculated using mathematical modelling so as to know the required quantities at any point in said trajectory, and an estimate of the integral flight load indicator during the "speed acceleration" exercise - IPLN1 - is obtained; 2) the "zoom climb" exercise, during performance whereof the optimal trajectory of the exercise is calculated using mathematical modelling so as to know the required quantities at any point in said trajectory, and the estimate of the integral flight activity indicator during the "zoom climb" exercise - IPLN2 - is calculated; 3) the "dive" exercise, during performance whereof the optimal trajectory of the exercise is calculated using mathematical modelling so as to know the required values at any point in said trajectory, and the estimate of the integral flight activity indicator during the "dive" exercise - IPLN3 - is obtained; 4) the "left turn" exercise, during performance whereof the optimal trajectory of the exercise is calculated using mathematical modelling so as to know the required quantities at any point in said trajectory, and the estimate of the integral flight activity indicator during the "left turn" exercise - IPLN4 - is obtained; 5) the "right turn" exercise, during performance whereof the optimal trajectory of performance is calculated using mathematical modelling, and the estimate of the integral flight activity indicator during the "right turn" exercise - IPLN5 - is obtained; 6) the "left ascending spiral" exercise, during performance whereof the optimal trajectory of the exercise is calculated using mathematical modelling so as to know the required quantities at any point in said trajectory, and the estimate of the integral flight activity indicator during the "left ascending spiral" exercise - IPLN6 - is obtained; 7) the "right descending spiral" exercise, during performance whereof the optimal trajectory of the exercise is calculated using mathematical modelling so as to know the required quantities at any point in said trajectory, and the estimate of the integral flight activity indicator during the "right descending spiral" exercise - IPLN7 - is obtained; then the arithmetic average value of the quantities IPLN1…IPLN7 is considered the estimate of the integral flight load indicator when performing the aerobatics complex IPLN, based on the quantity whereof the flight load is estimated as: "adequate", if the quantity UPLN does not exceed 0.5, "inadequate", if the quantity IPLN is in the range from 0.5 to 1, "substantially inadequate", if the quantity IPLN exceeds 1, considering that if the flight load is "inadequate", the pilot needs additional training in the exercise and psychophysiological training, and if the flight load is "substantially inadequate", the pilot is directed for a refresher training course or additional exercises with an instructor. 
     EFFECT: invention provides a possibility of evaluating the flight load of a helicopter pilot, accounting for the components of functional and professional reliability thereof. 
     1 cl, 28 tbl