Tangent Orbital Rendezvous Using Linear Relative Motion with <svg     style="vertical-align:-4.32007pt;width:18.525px;" id="M1" height="20.075001" version="1.1" viewBox="0 0 18.525 20.075001" width="18.525"  xmlns:xlink="http://www.w3.org/1999/xlink" xmlns="http://www.w3.org/2000/svg">
	
		
			<g transform="matrix(.022,-0,0,-.022,.062,14.637)"><path id="x1D43D" d="M434 650l-5 -28q-60 -8 -75 -20.5t-25 -69.5l-71 -395q-20 -107 -57.5 -168t-106.5 -94q-40 -18 -61 -20l-10 32q77 23 113 108q21 50 41 160l68 377q10 57 -1.5 69.5t-76.5 20.5l6 28h261z" /></g>

			<g transform="matrix(.016,-0,0,-.016,10.312,20.012)"><path id="x32" d="M412 140l28 -9q0 -2 -35 -131h-373v23q112 112 161 170q59 70 92 127t33 115q0 63 -31 98t-86 35q-75 0 -137 -93l-22 20l57 81q55 59 135 59q69 0 118.5 -46.5t49.5 -122.5q0 -62 -29.5 -114t-102.5 -130l-141 -149h186q42 0 58.5 10.5t38.5 56.5z" /></g>

		
	
</svg> Perturbations

<table>The flight-direction angle and the LVLH frame.</table>

Mathematical Problems in Engineering

fig1

Figure 1

Figure 1: Tangent Orbital Rendezvous Using Linear Relative Motion with <svg     style="vertical-align:-4.32007pt;width:18.525px;" id="M1" height="20.075001" version="1.1" viewBox="0 0 18.525 20.075001" width="18.525"  xmlns:xlink="http://www.w3.org/1999/xlink" xmlns="http://www.w3.org/2000/svg">
	
		
			<g transform="matrix(.022,-0,0,-.022,.062,14.637)"><path id="x1D43D" d="M434 650l-5 -28q-60 -8 -75 -20.5t-25 -69.5l-71 -395q-20 -107 -57.5 -168t-106.5 -94q-40 -18 -61 -20l-10 32q77 23 113 108q21 50 41 160l68 377q10 57 -1.5 69.5t-76.5 20.5l6 28h261z" /></g>

			<g transform="matrix(.016,-0,0,-.016,10.312,20.012)"><path id="x32" d="M412 140l28 -9q0 -2 -35 -131h-373v23q112 112 161 170q59 70 92 127t33 115q0 63 -31 98t-86 35q-75 0 -137 -93l-22 20l57 81q55 59 135 59q69 0 118.5 -46.5t49.5 -122.5q0 -62 -29.5 -114t-102.5 -130l-141 -149h186q42 0 58.5 10.5t38.5 56.5z" /></g>

		
	
</svg> Perturbations 

Mathematical Problems in Engineering

Tangent Orbital Rendezvous Using Linear Relative Motion with Perturbations

Figure 1