Question

Orbital Rendezvous: Assume that the Chief is in a circular orbit about the Earth with r_(c)= 6770km and mu =3.986 imes 10^(5)(km^(3))/(s^(2)). Given the initial conditions, x(t_(0))=[[x_(0)],[y_(0)],[z_(0)],[x_(0)^(˙)],[y_(0)^(˙)],[z_(0)^(˙)]]=[[-2.7613km],[.6191km],[1.9168km],[1(m)/(s)],[???],[-3(m)/(s)]] a. Use the HCW bounding condition to determine y_(0)^(˙) such that the relative orbit is bounded/periodic. b. What is the change in initial velocity needed to rendezvous at the same final position, 1 hour after t_(0) ? c. At time t_(f)=1 hour, what is the change in the final velocity need to match the velocity of the two spacecraft assuming the initial conditions computed in part b? 3. Orbital Rendezvous: Assume that the Chief is in a circular orbit about the Earth with re = Given the initial conditions -2.7613 kmj [xo] .6191 km yo 1.9168 km m X(to)= S ??? m 3 S a. Use the HCW bounding condition to determine Yo such that the relative orbit is bounded/periodic. b. What is the change in initial velocity needed to rendezvous at the same final position, 1 hour after to? c. At time tf = 1 hour, what is the change in the final velocity need to match the velocity of the two spacecraft assuming the initial conditions computed in part b?

          Orbital Rendezvous: Assume that the Chief is in a circular orbit about the Earth with r_(c)= 6770km and mu =3.986	imes 10^(5)(km^(3))/(s^(2)). Given the initial conditions,
x(t_(0))=[[x_(0)],[y_(0)],[z_(0)],[x_(0)^(˙)],[y_(0)^(˙)],[z_(0)^(˙)]]=[[-2.7613km],[.6191km],[1.9168km],[1(m)/(s)],[???],[-3(m)/(s)]]
a. Use the HCW bounding condition to determine y_(0)^(˙) such that the relative orbit is bounded/periodic.
b. What is the change in initial velocity needed to rendezvous at the same final position, 1 hour after t_(0) ?
c. At time t_(f)=1 hour, what is the change in the final velocity need to match the velocity of the two spacecraft assuming the initial conditions computed in part b?
3. Orbital Rendezvous: Assume that the Chief is in a circular orbit about the Earth with re = Given the initial conditions -2.7613 kmj [xo] .6191 km yo 1.9168 km m X(to)= S ??? m 3 S
a. Use the HCW bounding condition to determine Yo such that the relative orbit is bounded/periodic. b. What is the change in initial velocity needed to rendezvous at the same final position, 1 hour after to?
c. At time tf = 1 hour, what is the change in the final velocity need to match the velocity of the two spacecraft assuming the initial conditions computed in part b?

orbital rendezvous assume that the chief is in a circular orbit about the earth with rc 6770km and mu 3986times 105km3s2 given the initial conditions xt0x0y0z0x0 y0 z0 27613km6191km1 73075

Added by Jose J.

Question

Please give Ace some feedback