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 (42.2 KiB) Viewed 53 times

I Need Matlab Code For The Following Four Related 2nd Order Odes Please Provide Me The Clear Steps Let Us Consider The 2 (27.7 KiB) Viewed 53 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 hp = 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 l, = 1 = 100 m. R = 7371 km. P-0.1 mk-mR9² + 2. 3. μm R² 2mRRO +mR²0 +2m₁zl(+a)l cos² y + m₁21² (0+ a) cos²y (+a)y sin 2y] =-PR+ P cos y cos a (m₂l/m) 3μm₁₂1² 2R X (1-3 cos² a cos y) = 0 2m₁zl(+a)l cos² y + m₁21²[(+a) cos² y-2(+a)y cos y sin y] +3μ m121² sin 2a cos² y Pcos y cos a (m₂t/m) 2 R³ Notations: m₁l²y 2m₁lly + m²(+a) siny cosy + m12=m₁m₂/m m=m₂ + m₂ = GM 3μm₁21² R³ cos y sin y cos² a = - Psina sin y (™) M= mass of earth
N 2 Y R Debris Y Tug Tether C₁ 10 Anomaly (angle) The tug is a point mass; the debris may be a point mass or a finite-sized mass • Tug's thrust is low • Tether length is constant 17