Introducing Dimitar

IDEA: WE USE MATHEMATICAL SCRIPTS AND EQUATIONS TO DETERMINE THE OPTIMAL MOMENT IN TIME THAT BALANCES THE STRUCTURE OF A COSMIC OBJECT WITH ITS ASSOCIATED ENERGY (OR FREQUENCY), THUS ACHIEVING AN OPTIMAL STATE OF THE SYSTEM. THIS APPROACH CAN BE APPLIED IN VARIOUS SCENARIOS IN SPACE WHERE WE WANT TO DETERMINE THE EXACT MOMENT IN TIME WHEN SPECIFIC CONDITIONS ARE MET OR THE SYSTEM IS IN EQUILIBRIUM. FORMULAS AND SCRIPT: FORMULAS FOR STRUCTURE AND ASSOCIATED ENERGY/FREQUENCY: ​THE FUNCTION N(T) REPRESENTS THE STRUCTURE OF THE COSMIC OBJECT AND IS CALCULATED THROUGH AN EQUATION DEPENDENT ON PARAMETERS K , THE GRAVITATIONAL CONSTANT G, AND TIME T. THE FUNCTION F(T) REPRESENTS THE ASSOCIATED ENERGY (OR FREQUENCY) OF THE COSMIC OBJECT AND DEPENDS ON THE MASS M, THE SPEED OF LIGHT C, AND TIME T. SCRIPT: THE SCRIPT UTILIZES OPTIMIZATION TO FIND THE MINIMUM DIFFERENCE BETWEEN THE STRUCTURE AND ASSOCIATED ENERGY/FREQUENCY OF THE COSMIC OBJECT. THIS MINIMUM IS FOUND BY DETERMINING THE OPTIMAL MOMENT IN TIME THAT BALANCES THESE TWO FUNCTIONS. AFTER RUNNING THE SCRIPT, WE OBTAIN THE OPTIMAL MOMENT IN TIME THAT ACHIEVES EQUILIBRIUM OR AN OPTIMAL STATE OF THE COSMIC OBJECT. EXAMPLES: LAUNCHING A PROBE TO MARS: THE SCRIPT CAN DETERMINE THE OPTIMAL MOMENT FOR LAUNCHING A PROBE TO MARS, WHERE THE STRUCTURE OF THE PROBE AND ITS ASSOCIATED ENERGY (FREQUENCY) ARE IN BALANCE, MINIMIZING COSTS AND TRAVEL TIME. CHANGES IN THE ICY REGIONS OF MARS: THE SCRIPT CAN HELP US UNDERSTAND HOW THE WATER ICE ON MARS CHANGES AND ITS IMPACT ON THE THERMAL BALANCE BY DETERMINING THE OPTIMAL MOMENT IN TIME WHEN THESE CHANGES ARE IN EQUILIBRIUM. THIS OPTIMIZATION METHOD CAN BE APPLIED IN SPACE SCIENCES TO FIND THE PRECISE MOMENT IN TIME THAT ACCOMPLISHES DESIRED GOALS OR TASKS IN SPACE WHILE MAINTAINING A BALANCE BETWEEN THE SYSTEM'S STRUCTURE AND ASSOCIATED ENERGY/FREQUENCY.