I need MATLAB code for the following four related 2nd order ODES. Please provide me the clear steps. Let us consider the

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I Need Matlab Code For The Following Four Related 2nd Order Odes Please Provide Me The Clear Steps Let Us Consider The 1 (47.54 KiB) Viewed 67 times

I Need Matlab Code For The Following Four Related 2nd Order Odes Please Provide Me The Clear Steps Let Us Consider The 2 (63.92 KiB) Viewed 67 times

I need MATLAB code for the following four related 2nd order ODES. Please provide me the clear steps. Let us consider the motion of the system in a Keplerian orbit with semi-major axis 7371 km and eccentricity e = 0.05. These parameters correspond to the orbit with ha = 1369 km and h, = 631 km. The space tug of mass m₁ 500 kg and the debris of mass m₂ = 3000 kg are connected by a tether of length lo = 1 = 100 m. R = 7371 km. P-0.1 1. mk-mR9² + 2. 3. μm 3μm₁1² R² 2R¹ 2mRRO +mR²0 +2m,2l(+a)l cos² y + m2l²[(+a) cos² y-(+a)y sin 2y] =-PR + P cos y cos a (m₂l/m) -x (1-3 cos² a cos y) = 0 2m₁l(+a)l cos² y + m₁21²[(+a) cos² y 2(0+ a)y cos y siny] + Notations: m₁21² y 2m₁lly + m²(+a) siny cosy + m₁2=m₁m₂/m m-m, + m₂ 3μm₁21² R³ JL = GM 3μm121² 2 R³ sin 2a cos² y = P cos y cos a (m₂t/m) cos y sin y cos² a = -Psina sin y M= mass of earth (²) m
Z 2- Y R Debris Y Tug v X C₂ C Tether C₁ 87 P X