... launch and reentry , it is often tempting to use coordinates such as altitude and horizontal distance flown : the type of coordinates used to describe the flight of aircraft . Examine Figure 1.10 , where X is downrange distance flown ... Designed for undergraduate courses in Spacecraft Dynamics and Orbital Mechanics, this new edition offers a three-dimensional treatment of dynamics discussions of rigid body dynamics, rocket trajectories, and the space environment. An expert in his field, author William E. Wiesel presents a wealth of information in an easy-to-understand manner without the daunting mathematical rigor of graduate texts. Reference is made to actual flight vehicles and satellites to give students background on the type of work currently being done in this field. Dari dalam buku Ada 1 halaman yang cocok dengan Downrange distance is the horizontal distance traveled by a vehicle from the launch site dalam buku ini Halaman 19 Ke mana bagian lainnya buku ini? Isi Particle Dynamics 1 The TwoBody Problem 44 EarthSatellite Operations 73 Hak Cipta 10 bagian lainnya tidak diperlihatkan Edisi yang lain - Lihat semua Spaceflight Dynamics William E. Wiesel Tampilan cuplikan - 1989 Istilah dan frasa umum altitude angular momentum angular rate angular velocity angular-momentum vector angular-velocity vector astronaut atmosphere b₁ body frame booster burnout calculate center of mass circular orbit components constant coordinate cross product derivative differential equations direction dot product dynamics earth ellipse ellipsoid engines equations of motion Euler Euler's equations force fuel function geosynchronous orbit gimbal given gravity gyroscope Hohmann transfer hyperbola inertial acceleration inertial frame inertial navigation integral launch magnetic field maneuver moment-of-inertia matrix moon multistage rocket Newton's obtain particle perigee planet platform polhode position vector quantity r₁ radiation radius rate gyroscope reentry reference frame respect restricted problem rigid body rocket rotation matrix rotor satellite semimajor axis shown in Figure shuttle solar system solution space spacecraft speed spin stable stage term thrusters torque trajectory two-body problem unit vectors vehicle velocity vector vertical wbi vector zero Informasi bibliografi Judul Spaceflight Dynamics, Volume 1 Volume 100-101 dari Advances in the astronautical sciences McGraw-Hill series in aeronautical and aerospace engineering Pengarang William E.