
Optimal Control and Estimation Theory 523
to the desired final conditions
θ
(t
f
)=
θ
f
˙
θ
(t
f
)=
˙
θ
f
The loss function to be minimized is given by
J =
1
2
t
f
t
0
u
2
(t) dt
where this J is not to be confused with the inertia. We restrict attention to the case
that t
0
= 0andt
f
= T are fixed. Two methods are considered to derive the optimal
maneuver. First we note that direct substitution of the dynamics equation into the
loss function yields an equation of the form given by
ϑ
(
θ
,
˙
θ
,
¨
θ
, t)=
1
2
¨
θ
2
(t)
This form is not identical to the form presented in Equation (8.1); however, the exten-
sion of the Euler-Lagrange equations to higher-order derivatives is straightforward
(which ...